.The
127 spacecrafts launched in 1964:
..
Spacecraft
Entries
.
"Ferret"
Spacecraft: |
|
Chronologies: |
1964 payload #1 ; 1964-001A ; 353rd spacecraft. |
Type: |
Electronic intelligence |
Sponsor: |
U.S. Army & U.S. Navy |
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GGSE 1
Spacecraft: |
GGSE stands for Gravity Gradient
Stabilization Experiment ; S00728 NRL |
Chronologies: |
1964 payload #2 ; 1964-001B ; 354th spacecraft. |
Type: |
Technology |
Sponsor: |
U.S. Army & U.S. Navy |
|
|
Launch: |
11 January 1964, from Vandenberg
Air Force Base's LC-75-3-5, by a Thor-Agena D (Thor 2A 390 / Agena D 2354). |
Orbit: |
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Decayed: |
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Mission: |
GGSE-1 was a 39-kg technology satellite,
the first in the series that developed designs and deployment techniques
later applied to the NOSS/Whitecloud reconnaisance satellites. New
gravity gradient stabilization system utilizing earth‘s gravitational field
to orient the satellite and earth‘s magnetic field to assist in damping
was developed by General Electric and recently tested onboard a USN satellite,
orbited Jan. 11. Within three days the system stabilized the satellite
to accuracy of +/-5 degrees. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-001B
; TRW Space Log ; Astronautical
Events of 1964, p. 68 ; |
|
|
.
EGRS 1 / Secor 1
Spacecraft: |
SECOR stands for SEquential COllation
of Range |
Chronologies: |
1964 payload #3 ; 1964-001C ; 355th spacecraft. |
Type: |
Geodesy |
Sponsor: |
U.S. Army & U.S. Navy |
|
|
Launch: |
11 January 1964, from Vandenberg
Air Force Base's LC-75-3-5, by a Thor-Agena D (Thor 2A 390 / Agena D 2354). |
Orbit: |
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Decayed: |
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Mission: |
On 18 February 1964, Dr. Albert C. Hall,
Deputy Director for Space, Defense Research and Engineering, disclosed
that the Army had secretly launched SECOR last month and that it was performing
“exceptionally well.” On 21 February 1964, DOD announced Army Corps of
Engineers’ SECOR geodetic satellite was performing “exceptionally well,”
confirming Dr. Albert Hall’s disclosure of Feb. 18. The 18-kg satellite
was orbiting at about 950-km altitude in periods of about 100 min. SECOR
system tests were being conducted by Army’s Geodesy, Intelligence and Mapping
Research and Development Agency (GIMRADA), which had contracted for the
satellite from ITT Federal Laboratories. GIMRADA ground stations were measuring
distances by sending and receiving signals through satellite’s onboard
transponder, then acquiring ranging data for use in automatic data reduction
process by Army Map Service to determine station positions. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-001C
; TRW Space Log ; Astronautical
Events of 1964, p. 68, 74 ; |
|
|
.
Solrad 7A / GRAB
Spacecraft: |
SR 7A. |
Chronologies: |
1964 payload #4 ; 1964-001D ; 356th spacecraft. |
Type: |
Sun observations |
Sponsor: |
U.S. Army & U.S. Navy |
|
|
Launch: |
11 January 1964, from Vandenberg
Air Force Base's LC-75-3-5, by a Thor-Agena D (Thor 2A 390 / Agena D 2354). |
Orbit: |
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Decayed: |
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Mission: |
On 4 February 1964,
U.S. Committee for International Quiet Sun Year (IQSY) and USN announced
satellite to monitor solar x-ray emission, instrumented by Naval Research
Laboratory scientists, was launched recently to initiate continuous “watch
on the sun” during IQSY (1964-65). First signals from the satellite showed
the sun now is close to its minimum activity, reported NRL scientists Robert
W. Kreplin, Talbot A. Chubb, and Herbe& Friedman. Any solar activity
that occurs this year should be isolated and relatively uncomplicated,
permitting the satellite to record individual stonn centers, in contrast
to IGY which was marked by succession of overlapping storms. Observatories
in 14 countries joined U.S. in preparing to utilize continuous data transmissions
from the satellite. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-001D
; TRW Space Log ; Astronautical
Events of 1964, p. 45 ; |
|
|
.
GRAB 5
Spacecraft: |
|
Chronologies: |
1964 payload #5 ; 1964-001E ; 357th spacecraft. |
Type: |
Electronic intelligence |
Sponsor: |
U.S. Army & U.S. Navy |
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.
P-35-6 / DAPP 6
Spacecraft: |
OPS 3367A / AFP-43
Data Acquisition and Processing Program |
Chronologies: |
1964 payload #6 ; 1964-002B ; 358th spacecraft. |
Type: |
Technology |
Sponsor: |
U.S. Air Force |
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.
P-35-7 / DAPP 7
Spacecraft: |
OPS 3367B / AFP-43
Data Acquisition and Processing Program |
Chronologies: |
1964 payload #7 ; 1964-002C ; 359th spacecraft. |
Type: |
Technology |
Sponsor: |
U.S. Air Force |
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Relay 2
Spacecraft: |
Relay B (A-16) |
Chronologies: |
1964 payload #8 ; 1964-003A ; 360th spacecraft. |
Type: |
Communications |
Sponsor: |
• NASA-Office of Space Science Applications |
|
|
Launch: |
21 January 1964 at 21h15 UTC,
from Cape Canaveral's LC-17B, by a Delta DSV-3B (Thor Delta B 373
/ Delta 23). |
Orbit: |
2,088 km x 2,411 km x 46.3° x 195-min. |
Decayed: |
|
Mission: |
Relay II is a 83.5-kg active communications
satellite that continues communications tests of Relay I, still in orbit,
and which provides evaluation of improvements in the new comsat. It is
equipped for transmitting one-way wideband communications (one-way TV,
300 one-way voice channels or high-speed data) or two-way narrow-band communications
(12 two-way telephone conversations or teletype, photo-facsimile and data).
Unlike its predecesor, It had no automatic cutoff device and is equipped
with solar cells with greater resistance to radiation than Relay 1’s cells.
Relay II was 22nd straight launch success of Thor-Delta launch vehicle.
Relay II completed
its first communications test during its first orbit, receiving radio signals
and TV test pattern from Mojave, Calif., ground station and beaming them
back to earth. First intercontinental communications tests conducted with
Relay II communications satellite, on 22 January 1964, were successful:
NASA officials described the satellite’s performance as “excellent.»
The tests were conducted between ground stations at Nutley, N.J., and Raisting,
West Germany, consisted of voice transmissions and radio signals.
On 29 January 1964,
Relay II transmitted portions of Soviet-American championship hockey game
of the 1964 Winter Olympics at Innsbruck, Austria, to the U.S., the first
public demonstration of Relay II. By this time numerous communications
tests of the satellite had been made, and NASA scientists said that all
communications experiments were of excellent quality. The satellite was
also was sending back information on radiation collected by onboard instrumentation.
On 25 March 1964,
first TV transmission from Japan to U.S. was made, using NASA’s Relay II
communications satellite. Quality of the live pictures as well as the sound
was excellent. In the telecast Prime Minister Hayato Ikeda offered his
country’s apologies directly to the U.S. for the “unfortunate coincidence”
of the stabbing of U.S. Ambassador Edwin Reischauer by a deranged Japanese
youth the previous day. The eight-minute telecast was seen simultaneously
on the three national networks.
Relay 2 was a 184-kg communications satellite.
Physically similar to Relay 1, it had on board two transmitters.
The satellite was spin-stabilized and also carried particle experiments
designed to map the trapped. Design changes in Relayd 2 improved its performance
to the point where response to spurious commands was essentially eliminated.
One of the two onboard transponders operated normally until 20 November
1966. The other transponder continued to operate until9 June
1967. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-003A
; TRW Space Log ; Astronautical
Events of 1964, p. 19-20, 22, 32, 115 ; |
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Echo 2
Spacecraft: |
Echo C (A-12) |
Chronologies: |
1964 payload #9 ; 1964-004A ; 361st spacecraft. |
Type: |
Communications |
Sponsor: |
NASA-Office of Space Science Applications |
|
|
Launch: |
25 January 1964 at 13h59 UTC,
from Vandenberg Air Force Base's LC-75-1-1, by a Thor-Agena B (Thor 397
/ Agena B 6301 (TA2)). |
Orbit: |
1,033 km x 1,313 km x 81.5° x 109 min. |
Decayed: |
7 June 1969. |
Mission: |
Echo II is a 243-kg passive communications
satellite, a 41-metre diameter, laminated mylar plastic and aluminum balloon.
for testing propagation, tracking, and communication techniques. It was
a 41-metres balloon of aluminum foil-mylar laminate. Instrumentation included
a beacon telemetry system that provided a tracking signal, monitored spacecraft
skin temperature and internal pressure. In addition to fulfilling its communications
mission, the spacecraft was used for global geometric geodesy. Soviet
ground stations were tracking Echo II passive communications satellite,
in first joint U.S.-U.S.S.R. space experiment. The spacecraft re-entered
the atmosphere on June 7, 1969. |
Notes: |
On 12 August 1963, NASA announced G.C. Schieldahl
Co. had been selected to build Echo II satellite, scheduled to be placed
in orbit during the 1963-64 winter. Under $362,000 contract, Schieldahl
would build three models, one for static-inflation tests, one for orbital
flight. and one for back-up. Echo II would be larger and more rigid than
its predecessor, Echo 1.
Early telemetry
and radar reports indicated Echo II appeared to be losing its spherical
shape and high reflectivity, NASA spokesman announced. Telemetry showed
Echo II pressure “has decreased more rapidly than anticipated.” However,
“optical observations tell us we have a beautiful balloon.” Analysis of
TV photographs taken by camera mounted on Agena stage showed sphere had
inflated properly; but inflating gas apparently leaked out after two hours
instead of lasting for 20 hours as planned. However, quality of radio signals
between Rome, N.Y., and reported to be good. Spokesman indicated telemetry
reports of pressure decrease could be false due to possible error in the
observations.
On 29 January 1964,
NASA spokesman said Echo II balloon satellite was still operating with
“great success” despite preliminary radar reports that it was deflating
and losing its reflectivity. On 29 February 1964, Echo II was used
for transmission of two radiophotos between Britain’s Jodrell Bank Experimental
Station at Manchester and Gorki University’s radioastronomy observatory
at Zimenki. A third space telegram was sent from Jodrell Bank to Zimenki
via the moon, and its quality was comparable to those received via Echo
II. The U.S. satellite was termed by Tass commentator “the Friendship Sputnik.” |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-004A
; TRW Space Log ;
Astronautical Events of 1963, p. 305 ; Astronautical
Events of 1964, p. 24, 27, 30, 33, 85 ; |
|
|
.
Saturn SA-5
Spacecraft: |
|
Chronologies: |
1964 payload #10 ; 1964-005A ; 362nd spacecraft. |
Type: |
Technology |
Sponsor: |
NASA-Office of Manned Space Flight |
|
|
Launch: |
29 January 1964 at 16h25 UTC,
from Cape Canaveral's LC-37B, by a Saturn I (SA-5). |
Orbit: |
269 km x 755 km |
Decayed: |
|
Mission: |
Saturn I SA-5 was a launch vehicle development
test. It was the fifth flight of a Saturn rocket and the first of
the Block II Saturn. It was also the first live flight of the LOX/LH2 fueled
second stage (S-IV). More than 11,000 measurements were taken. (Mass: 17554.2
kg)
Saturn I SA-5 was
first successful flight test of both stages of the rocket. The 680-ton-thrust
S-I stage performed as planned, and the 40-ton-thrust upper stage (S-IV)
powered by six liquid-hydrogen RL-10 engines separated and burned properly
for eight minutes, attaining orbital speed. The orbited body (spent S-IV
stage, instrument unit, payload adapter, Jupiter nose cone, and 5,200 kg
of sand ballast) weighed 17,100 kg, nearly 9,000 kg of which was payload.
As the first of
the Block II Saturn I’s, SA-5 was first flight test of both Saturn stages
and only the second flight test of a liquid-hydrogen powered rocket stage
(after Centaur AC-2, on 27 November 1963). The five Block II Saturn 1’s
differ from Block I predecessors in that they have live upper stages, S-I
propellant tanks are extended to provide 45,000 kg usable propellant, and
tail fins are added for stability.
During the flight
eight onboard motion picture cameras photographed various operations of
the rocket and a TV camera provided real-time photographs of separation
and ignition of S-IV stage. Shortly after S-I burnout, the motion picture
cameras were ejected, impacting downrange where pararescue men recovered
seven of them.
This test of the
world’s largest known rocket proved flight capability of Saturn I’s liquid-hydrogen,
clustered-engine upper stage and demonstrated the vehicle’s capability
to orbit 20,000-lb. [9-ton] payload.
Preliminary evaluation
of Saturn I SA-5 flight indicated there was “no significant deviation or
malfunction.”. Because insertion velocity was slightly greater than predicted,
the 19,100 kg orbiting body was in an earth orbit slightly higher than
expected: apogee 100-km higher than expected and perigee 10=km higher than
expected. Timing of all significant actions in the launch sequence vaned
no more than half a second from prediction. First stage cutoff occurred
after slightly more than 146 sec., S-IV stage ignited at 148 sec., and
insertion into orbit occurred at 639 sec. [10 min. 39 sec].
Following
successful launching of Saturn I two-stage SA-5, President Johnson issued
statement saying U.S. had now “proved we have the capability of putting
great payloads into space.…
“We have come a
long way from the 14 kg of Explorer I on January 31, 1958, to the some
16,700 kg which has just been placed into orbit by Saturn I.
“We have demonstrated
not only enormous boost capability, but we have proved the effectiveness
and the practical use of liquid hydrogen as a rocket fuel for space flight…”
NASA Associate Administrator,
Dr. Robert C. Seamans stated, “There is little question that it took us
ahead of the Russians in our capability.” He noted that payload equivalent
of SA-5’s orbiting body was between 8,600 to 9,000 kg, far exceeding the
6,482 kmg reported for heaviest Soviet satellites.
Rep. J. Edward Roush
(D.-Ind.) said in the House: “On Wednesday we saw the successful launching
of the Saturn rocket carrying into orbit around the earth 18 tons. This
included the largest payload ever placed in orbit by man and exceeds the
largest Russian payload by 11 tons. For several years now this Nation has
been plagued with the uncomfortable knowledge that the Russians were ahead
of us in the space effort. This has been based primarily on the fact that
they had a greater lift capability. The United States is now ahead in lift
capability and in every other phase of the space program.…” |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-005A
; TRW Space Log ; Astronautical
Events of 1964, p. 32, 35, 49 ; |
|
|
.
Elektron 1
Spacecraft: |
2D No. 1 |
Chronologies: |
1964 payload #11 ; 1964-006A ; 363rd spacecraft. |
Type: |
Earth upper atmosphere studies |
Sponsor: |
Soviet Union |
|
|
Launch: |
30 January 1964 at 9h45 UTC,
from Baykonur Cosmodrome, by an A-1/"Vostok" (8A92). |
Orbit: |
406 km x 7,100 km x 61° x 2-hr. 49-min. |
Decayed: |
|
Mission: |
Electron 1 was launched with Electron 2 by
a single launch vehicle in order to perform simultaneous investigations
of the external and internal zones of the Earth's radiation belt. Soviet
news agency Tass said the satellites were studying “the internal and external
radiation belts of the earth and physical phenomena connected with them.”
The 350-kg spacecraft had a cylindrical body that was 0.75 m in diameter
and 1.3 m long and from which antennas and six solar cell panels were extended.
The spacecraft was placed into an eccentric orbit that enabled it to study
the internal zone of the radiation belt. It was equipped with micrometeorite
detectors, a mass spectrometer, a proton detector, and instruments for
recording the corpuscular emission and energy spectrum of electrons. A
memory device was included so that observations over several orbits could
be obtained by Soviet telemetry stations when the satellite was within
communications range.
On 2 February 1964,
Tass announced Electron I and Electron II scientific satellites were continuing
their elliptical orbits of the earth. By 6:00 p.m. Moscow time Feb. 1,
Electron I had passed repeatedly through the inner radation belt in its
19 orbits and Electron II had moved four times through the outer radiation
belt in its two orbits. Tass said the following studies were being made
with aid of onboard equipment: outer and inner radiation belts; charged
particles having low energy; concentrations of electrons and positive ions;
magnetic fields and radiation belts of the earth; nuclear component of
cosmic radiation; shortwave solar radiation; propagation of radio waves;
radio-radiation of galaxies; and densities of meteoritic material. Tass
said the studies, being accomplished under a unified program in various
areas of outer space, were being conducted for the first time. These studies
were important for conducting the program of the IQSY and for permitting
collection of data to assure radiation safety of manned space flights.
Tass said all onboard equipment was functioning normally and ground stations
were receiving scientific data from the satellites. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-006A
; TRW Space Log ; Astronautical
Events of 1964, p. 35, 43, 54, 62 ; |
|
|
.
Elektron 2
Spacecraft: |
2D No. 2 |
Chronologies: |
1964 payload #12 ; 1964-006B ; 364th spacecraft. |
Type: |
Earth upper atmosphere studies |
Sponsor: |
Soviet Union |
|
|
Launch: |
30 January 1964 at 9h45 UTC,
from Baykonur Cosmodrome, by an A-1/"Vostok" (8A92). |
Orbit: |
460 km x 68,200 km x 61° x 22-hr. 40-min. |
Decayed: |
|
Mission: |
Electron 2 was launched with Electron 1 by
a single launch vehicle in order to perform simultaneous investigations
of the external and internal zones of the Earth's radiation belt. Soviet
news agency Tass said the satellites were studying “the internal and external
radiation belts of the earth and physical phenomena connected with them.”
The 445-kg spacecraft had a cylindrical body that was 0.75 m in diameter
and 1.3 m long and from which antennas and six solar cell panels were extended.
The spacecraft was placed into an eccentric orbit that enabled it to study
the internal zone of the radiation belt. It was equipped with micrometeorite
detectors, a mass spectrometer, a proton detector, and instruments for
recording the corpuscular emission and energy spectrum of electrons. A
memory device was included so that observations over several orbits could
be obtained by Soviet telemetry stations when the satellite was within
communications range.
On 2 February 1964,
Tass announced Electron I and Electron II scientific satellites were continuing
their elliptical orbits of the earth. By 6:00 p.m. Moscow time Feb. 1,
Electron I had passed repeatedly through the inner radation belt in its
19 orbits and Electron II had moved four times through the outer radiation
belt in its two orbits. Tass said the following studies were being made
with aid of onboard equipment: outer and inner radiation belts; charged
particles having low energy; concentrations of electrons and positive ions;
magnetic fields and radiation belts of the earth; nuclear component of
cosmic radiation; shortwave solar radiation; propagation of radio waves;
radio-radiation of galaxies; and densities of meteoritic material. Tass
said the studies, being accomplished under a unified program in various
areas of outer space, were being conducted for the first time. These studies
were important for conducting the program of the IQSY and for permitting
collection of data to assure radiation safety of manned space flights.
Tass said all onboard equipment was functioning normally and ground stations
were receiving scientific data from the satellites. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-006B
; TRW Space Log ; Astronautical
Events of 1964, p. 35, 43, 54, 62 ; |
|
|
.
Ranger 6
Spacecraft: |
RA-6 |
Chronologies: |
1964 payload #13 ; 1964-007A ; 365th spacecraft. |
Type: |
Lunar probe |
Sponsor: |
NASA |
|
|
Launch: |
30 January 1964 at 15h49 UTC,
from Cape Canaveral's LC-12, by an Atlas-Agena B (Atlas LV-3A 199D / Agena
B 6008). |
Orbit: |
Earth-Moon trajectory. |
Decayed: |
2 February 1964 (impacted on the Moon). |
Mission: |
Ranger VI was a 365-kg lunar probe that would
impact the lunar surface. The only scientific instruments onboard spacecraft
were six TV cameras, designed to provide more than 3,000 photographs of
the lunar surface during the last 10 min. of the 66-hr. flight. This was
the first Ranger launch since October 1962, when extensive review of the
Ranger project was undertaken because of previous Ranger failures. For
Ranger VI, changes were made in subsystems to improve reliability and provide
redundancy in some areas; also, sterilization requirements for Ranger spacecraft
were relaxed, since excessive heat was suspected of causing some previous
malfunctions. Target for the lunar spacecraft: Sea of Tranquility.
On 2 February 1964,
Ranger VI crashed onto the moon on target in the Sea of Tranquility, but
its onboard camera system failed to return TV photographs of the lunar
surface. Indications were that the two TV systems responded to Central
Computer and Sequencer (CCS~Sc) command to warm up, but the cameras did
not complete the warm-up to picture taking. Ranger VI’s cameras (two wide-angle
and four narrow-angle) were to have made more than 3,000 photographs during
its last 10 min. The photographs were to have provided scientific data
on lunar topography and supported the Surveyor unmanned soft-landing spacecraft
and Apollo manned lunar landing program. Sir Bernard Lovell, Director of
Jodrell Bank Experimental Station which tracked Ranger VI on its course
to the moon, said of the spacecraft’s accurate impact of the moon: “I think
this represents a very great achievement for American rocket engineers.
“This achievement is underlined by the fact that it is now four and a half
years since either the Russians or the Americans have made a direct hit
of this nature on the lunar surface, despite repeated attempts. NASA planned
three more Ranger TV flights this year. Ranger VI impacted the moon
withing 30-km of its target and within one third of a second of the predicted
afrival time.
On 2 April 1964,
NASA Administrator, James E. Webb, detailed possible causes of failure
of Ranger VI. Although not yet identified any specific cause for failure
were identified, Mr. Webb outlined five major faults in the spacecraft:
1. The two oaboard TV systems “were more complex than required and were
not completely redundant. They included a number of common components in
which a single failure would lead to disablement of both television systems.”
2. “Possibilities of failure… increased as a result of practices employed
in the design and construction of the spacecraft.…” 3. Preflight ground
testing “may have obscured potentially dangerous situations which could
have enhanced accidental triggering of critical control circuits.” 4. The
antenna for transmitting the lunar photographs had never been tested with
the TV transmitters. 5. “Because of reluctance to risk possible damage
to the space vehicle, pre-launch systems verification was not complete.…”
On 27 April 1964, Dr. Homer E. Newell, NASA
Associate Administrator for Space Sciences and Applications, said before
House Subcommittee on NASA Oversight about Project Ranger:
”… From the outset, the concept was advanced.
It was conceived to seize the initiative in space exploration from the
Soviet as well as to obtain important information about the moon. Had it
succeeded, it certainly would have been a major first for this country,
and it may still obtain that objective. The spacecraft itself is quite
complex.… It is comparable to the most sophisticated launch vehicles in
terms of electromechanical system complexity. Launch vehicles developed
in this country have typically taken 20 or more flights to achieve 50%
reliability. Some have not done much better than this after many more firings.
Indeed, we have read recently that last year there were 13 consecutive
failures of the Atlas. In addition, the Discoverer project took 13 attempts
to recover its first payload from orbit. Polaris experienced 5 initial
failures before its first success. Skybolt experienced 5 flights without
achieving complete mission success. In each of these projects, partial
success in early flights helped improve later flights. Although I believe
Skybolt was dropped for other reasons, Atlas, Discoverer, and Polaris all
went on to become vital elements in the defense posture of this country.
“Ranger is going through this same process.
We have solved some of our launch vehicle problems to the point where the
reliability is improving appreciably. The basic spacecraft bus has been
retained and has now demonstrated its capabiIity to deliver a payload to
a precise spot on the lunar surface. We now must make the payload work.
The payload also is pushing the state of the art in high power television
telemetry. This was necessary to obtain high resolution photographs… Our
reviews of the Ranger system continue to convince us of its capability
of performing the mission. While we how we cannot have100% reliability
with launch vehicle, spacecraft, or payload, we expect to achieve at least
one complete success with the remaining three flights.…
“Ranger is a tough job. Although success has eluded us, it is within
our grasp. We must have the fortitude to proceed. Space will only be conquered
by those who do have such fortitude. It might be well to point out that
our competitors in this area of exploration are not lacking in this respect.
It is reported that the Soviet Union has failed in from 15 to 20 consecutive
lunar and planetary mission attempts since Lunik IIIphotographed the back
side of the moon in 1959.
“Even should subsequent Rangers fail through unforeseen causes, we
must move ahead. We must look at the totality of the space program. … The
over-all picture is very good and is most convincing of this country’s
capability to successfully complete these undertakings. The trends are
all in our favor.…”
Ranger 6 was a 381-kg planetary probe designed
to achieve a lunar impact trajectory in order to transmit high-resolution
photographs of the lunar surface during the final minutes of flight.
It carried six television vidicon cameras. The
cameras were arranged in two separate chains, each self-contained with
separate power supplies, timers, and transmitters so as to affordthe greatest
reliability and probability of obtaining high-quality video pictures. No
other experiments were carried on the spacecraft.
It was the first
so-called Block 3 versions of the Ranger spacecraft. The spacecraft consisted
of a hexagonal aluminum frame base 1.5 metre across on which was mounted
the propulsion and power units, topped by a truncated conical tower which
held the TV cameras. Two solar panel wings, each 73.9 cm wide by 153.7
cm long, extended from opposite edges of the base with a full span of 4.6
m, and a pointable high gain dish antenna was hinge mounted at one of the
corners of the base away
from the solar panels. The overall height
of the spacecraft was 3.6 m.
On February 2, 1964,
65.5 hours after launch, Ranger 6 impacted the Moon on the eastern edge
of Mare Tranquillitatis (Sea of Tranquility)
at 9.358° North, 21.480° East. The
orientation of the spacecraft to the surface during descent was correct,
but no video signal was received and no camera data obtained. A review
board determined the most likely cause of failure was due to an arc-over
in the TV power system when it inadvertently turned on for 67 seconds approximately
2 minutes after launch during the period of booster-engine separation. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-007A
; TRW Space Log ; Astronautical
Events of 1964, p. 34-5, 36, 41, 61, 126, 150-1 ; |
|
|
.
Discoverer 72 / CORONA
1004 / KH-4A
Spacecraft: |
OPS 3444 |
Chronologies: |
1964 payload #14 ; 1964-008A ; 366th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Zond
Spacecraft: |
3MV-1 No. 2 SA |
Chronologies: |
1964 payload #15 ; 1964 1st loss ; 367th
spacecraft. |
Type: |
Venus probe |
Sponsor: |
Soviet Union (Korolev's Design Bureau) |
|
|
Launch: |
19 February 1964 at 5h47 UTC,
from Baykonur Cosmodrome's LC-1, by an A-2-e/"Molniya" (8K78M). |
Orbit: |
|
Decayed: |
|
Mission: |
U.S.S.R.’s unsuccessful attempts to send
payloads to Venus Feb. 26 and Mar. 4 were reported in the U.S. press on
30 March 1964. Failures were attributed by U.S. military officials to difliculties
with upper-stage rocket supposed to send the spacecraft out of parking
orbit and onto its interplanetary course |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; TRW Space Log ; Astronautical
Events of 1964, p. 120, ; |
|
|
.
Improve Samos 5 / KH-7
5
Spacecraft: |
OPS 2423 ; AFP-206 SV 955 |
Chronologies: |
1964 payload #16 ; 1964-009A ; 368th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Kosmos 25
Spacecraft: |
DS-P1 No. 4 |
Chronologies: |
1964 payload #17 ; 1964-010A ; 369th spacecraft. |
Type: |
Antimissile technologies |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Ferret 5
Spacecraft: |
OPS 3722 |
Chronologies: |
1964 payload #18 ; 1964-011A ; 370th spacecraft. |
Type: |
Electronic intelligence |
Sponsor: |
U.S. Air Force |
|
|
|
.
Improve Samos 6 / KH-7
6
Spacecraft: |
OPS 3435 ; AFP-206 SV 956 |
Chronologies: |
1964 payload #19 ; 1964-012A ; 371st spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Kosmos 26
Spacecraft: |
DS-MG No. 1 |
Chronologies: |
1964 payload #20 ; 1964-013A ; 372nd spacecraft. |
Type: |
Earth upper atmosphere studies (civil) |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Beacon Explorer A
Spacecraft: |
BE-A / S-66 |
Chronologies: |
1964 payload #21 ; 1964 2nd loss ; 373rd
spacecraft. |
Type: |
Earth upper atmosphere studies |
Sponsor: |
NASA |
|
|
Launch: |
19 March 1964 at 11h14 UTC, from
Cape Canaveral's LC-17A, by a Delta DSV-3B (Thor Delta B 391 / Delta 24). |
Orbit: |
n/a |
Decayed: |
n/a |
Mission: |
Beacon satellite (5-66) was a 55-kg satellite
designed to transmit data on the ionosphere directly to worldwide network
of ground stations. In addition to making major ionosphere studies, the
satellite was to have served as test bed for two geodesic experiments:
reflection of a laser beam directed from Wallops Island, Va., and transmission
on two frequencies permitting ground stations to study Doppler method of
satellite tracking and influence of ionosphere on Doppler tracking. The
attempt to orbit the satellite failed when third stage of Delta launch
vehicle burned for only 22 sec. instead of normal 40. This was only the
second Delta failure and followed 22 consecutive successes. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's EXP-66A
; TRW Space Log ; TRW Space Log ; Astronautical
Events of 1964, p. 109 ; |
|
|
.
Luna
Spacecraft: |
E-6 No. 4 SA |
Chronologies: |
1964 payload #22 ; 1964 3rd loss ;
374th spacecraft. |
Type: |
Lunar probe |
Sponsor: |
Soviet Union (Korolev's Design Bureau) |
|
|
|
.
Discoverer 73 / CORONA
1003 / KH-4A
Spacecraft: |
OPS 3467 |
Chronologies: |
1964 payload #23 ; 1964 4th loss ; 375th
spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
ORBIS 1
Spacecraft: |
|
Chronologies: |
1964 payload #24 ; 1964 5th loss ; 376th
spacecraft. |
Type: |
Technology? |
Sponsor: |
U.S. Air Force? |
|
|
|
.
Kosmos 27
Spacecraft: |
3MV-1 No. 3 SA |
Chronologies: |
1964 payload #25 ; 1964-014A ; 377th spacecraft. |
Type: |
Venus probe |
Sponsor: |
Soviet Union (Korolev's Design Bureau) |
|
|
Launch: |
27 March 1964 at 3h24 UTC, from
Baykonur Cosmodrome's LC-1, by an A-2-e/"Molniya" (8K78M T15000-22). |
Orbit: |
192 km X 237 km x 64.8° x 88.7-min. |
Decayed: |
|
Mission: |
“Soviet news agency Tass said that Cosmos
XXVII carried scientific instrumentation intended for the “further study
of outer space in accordance with the program announced by Tass” March
16, 1962, as well as radio transmitter and telemetering systems. All onboard
equipment was functioning normally.”
U.S.S.R.’s unsuccessful
attempts to send payloads to Venus Feb. 26 and Mar. 4 were reported in
the U.S. press on 30 March 1964. Failures were attributed by U.S. military
officials to difliculties with upper-stage rocket supposed to send the
spacecraft out of parking orbit and onto its interplanetary course. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-014A
; TRW Space Log ; Astronautical
Events of 1964, p. 114, 120 ; |
|
|
.
Ariel 2
Spacecraft: |
UK-C |
Chronologies: |
1964 payload #26 ; 1964-015A ; 378th spacecraft. |
Type: |
Astronomy |
Sponsor: |
United Kingdom |
|
|
Launch: |
27 March 1964 at 17h25 UTC, from
Wallops Island's LA-3, by a Scout (X-3 S127R). |
Orbit: |
290 km X 1,356 km x 52° x 101-min. |
Decayed: |
|
Mission: |
Ariel II is the second in series of three
U.S.-U.K. Earth sciences satellites.Under overall administrative responsibility
of the British Office of the Minister for Science, the three onboard experiments
were designed and built by the U.K. to measure vertical distribution of
ozone in the upper atmosphere, measure galactic radio noise, and detect
micrometeoroids encountered by the satellite. The experiments were chosen
by the British National Committee on Space Research, chaired by Sir Harrie
Massey, in consultation with NASA. NASA Goddard Space Flight Center built
and tested the spacecraft and contracted with Westinghouse Electric Corp.
for subsystems. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-015A
; TRW Space Log ; Astronautical
Events of 1964, p. 114 ; |
|
|
.
Zond 1
Spacecraft: |
3MV-1 No. 4 SA |
Chronologies: |
1964 payload #27 ; 1964-016A ; 379th spacecraft. |
Type: |
Venus probe |
Sponsor: |
Soviet Union (Korolev's Design Bureau) |
|
|
Launch: |
2 April 1964 at 2h52 UTC, from
Baykonur Cosmodrome, by an A-2-e/"Molniya" (8K78M T15000-23). |
Orbit: |
|
Decayed: |
|
Mission: |
U.S.S.R. launched Zond I space probe “for
the purppose of developing a space system for distant interplanetary flights.”
Final stage of “improved booster rocket” placed earth satellite into parking
orbit; then a rocket took off from the satellite and propelled the Zond
I to escape velocity, sending it into flight trajectory “close to the computed
one.” There was no indication as to what the computed course was, and no
details of the probe’s weight, size, or destination were given. The
probe was said to be in a flight trajectory corresponding “with a high
degree of accuracy” to the predetermined program. Soviet scientist Sergei
Vernon said at Moscow press conference that the Zond I space probe was
launched to study radiation hazards in space. The probe would “provide
information about more remote areas of space we know little about.”
On 15 April 1964,
Soviet news agency Tass said 25 communication sessions had been held with
Zond I since April 2, and a great deal of “interesting experimental data”
on the operation of onboard systems and individual units had been obtained.
By 6:00 pm., Moscow time, Zond I had reached 4,250,000 km from earth. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-016A
; TRW Space Log ; Astronautical
Events of 1964, p. 124, 127, 128, 131, 138 ; |
|
|
.
Kosmos 28
Spacecraft: |
Zenit-2 No. 16 |
Chronologies: |
1964 payload #28 ; 1964-017A ; 380th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
Launch: |
4 April 1964 at 9h36 UTC, from
Baykonur Cosmodrome's LC-31, by an A-1/"Vostok" (8A92). |
Orbit: |
209 km x 395 km x 65°x 90.38 min. |
Decayed: |
|
Mission: |
“U.S.S.R. announced routine launching of
Cosmos XXVIII. Scientific equipment onboard the satellite was “intended
for the further exploration of outer space in accordance with the program
announced by Tass March 16, 1962.” In addition, the satellite contained
radio transmitter and telemetering system. All instrumentation was functioning
normally.” |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-017A
; TRW Space Log ; Astronautical
Events of 1964, p. 128 ; |
|
|
.
Gemini 1
Spacecraft: |
Gemini spacecraft 1 |
Chronologies: |
1964 payload #29 ; 1964-018A ; 381st spacecraft. |
Type: |
Piloted spacecraft test |
Sponsor: |
NASA |
|
|
Launch: |
8 April 1964 at 16h00 UTC, from
Cape Canaveral's LC-19, by a Titan 2 (GLV GT-1). |
Orbit: |
160 km x 328 km x x 89.27 min. |
Decayed: |
12 April 1964 |
Mission: |
Titan II launched unmanned Gemini spacecraft
into orbit in first Project Gemini flight (GT-1), a test of Titan II launch
vehicle system, Gemini spacecraft structural integrity, and spacecraft-launch
vehicle compatibility. After an uninterrupted countdown at Cape Kennedy,
the Titan II lifted off and placed the spacecraft in orbit. Walter C. Willianis
said all systems functioned “well within manned tolerances.” Only imperfection
in the flight was Titan II’s 22.5 km/h excess speed (28,212 instead of
28,190 km/h), sending spacecraft 34 km higher than planned. However, this
was within tolerance and, on manned flight, crewmen could easily correct
the extra height. The 3,200 kg spacecraft was not separated from the spent
rocket casing. The spacecraft re-entered the earth’s atmosphere on
12 April 1964 and disintegrated midway between South America and Africa. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-018A
; TRW Space Log ; Astronautical
Events of 1964, p. 128, 134 ; |
|
|
.
Polyot 2
Spacecraft: |
I-2B No. 2 |
Chronologies: |
1964 payload #30 ; 1964-019A ; 382nd spacecraft. |
Type: |
Technology (ASAT) |
Sponsor: |
Soviet Union's Defense ministry |
|
|
Launch: |
12 April 1964 at 9h21 UTC, from
Baykonur Cosmodrome's, by a Polyot (11A59). |
Orbit: |
|
Decayed: |
|
Mission: |
Purposes of the steerable Polet II spacecraft
were said to be to “further improve space vehicles capable of maneuvering
extensively in all directions, and to work out questions concerning the
problem of space rendezvous.” After being placed in initial orbit, Polet
II was maneuvered in various directions by means of special engine system.
“As a result of one of these maneuvers in the area of the equator, the
space vehicle substantially changed the angle of inclination of its orbital
plane.” After the programed space maneuvers, Polet II was in a 310 x 500
km orbit, inclined at 58.06 degrees to the equator, and with an orbital
period of 92.4 min. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-019A
; TRW Space Log ; Astronautical
Events of 1964, p. 134 ; |
|
|
.
Luna
Spacecraft: |
ALS / E-6 No. 5 SA |
Chronologies: |
1964 payload #31 ; 1964 6th loss ; 383rd
spacecraft. |
Type: |
Lunar probe |
Sponsor: |
Soviet Union (Korolev's Design Bureau) |
|
|
|
.
Transit 5BN3
Spacecraft: |
|
Chronologies: |
1964 payload #32 ; 1964 7th loss ; 384th
spacecraft. |
Type: |
Navigation |
Sponsor: |
U.S. Navy |
|
|
|
.
Transit 5E2
Spacecraft: |
Transit VE-2 |
Chronologies: |
1964 payload #33 ; 1964 8th loss ; 385th
spacecraft. |
Type: |
Navigation |
Sponsor: |
U.S. Air Force |
|
|
|
.
Improve Samos 7 / KH-7
7
Spacecraft: |
OPS 3743 ; AFP-206 SV 957 |
Chronologies: |
1964 payload #34 ; 1964-020A ; 386th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Kosmos 29
Spacecraft: |
Zenit-2 No. 19 |
Chronologies: |
1964 payload #35 ; 1964-021A ; 387th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Discoverer 74 / CORONA
1005 / KH-4A
Spacecraft: |
OPS 2921 |
Chronologies: |
1964 payload #36 ; 1964-022A ; 388th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Kosmos 30
Spacecraft: |
Zenit-4 |
Chronologies: |
1964 payload #37 ; 1964-023A ; 389th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Improve Samos 8 / KH-7
8
Spacecraft: |
OPS 3592 ; AFP-206 SV 958 |
Chronologies: |
1964 payload #38 ; 1964-024A ; 390th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Apollo SA-5
Spacecraft: |
Apollo BP-13 |
Chronologies: |
1964 payload #39 ; 1964-025A ; 391st spacecraft. |
Type: |
Piloted spacecraft test |
Sponsor: |
NASA |
|
|
|
.
Molniya-1 No 2
Spacecraft: |
|
Chronologies: |
1964 payload #40 ; 1964 9th loss ; 392nd
spacecraft. |
Type: |
Communications |
Sponsor: |
Soviet Union |
|
|
|
.
Transit 5C1
Spacecraft: |
Transit VC |
Chronologies: |
1964 payload #41 ; 1964-026A ; 393rd spacecraft. |
Type: |
Navigation |
Sponsor: |
U.S Navy |
|
Source: A.
Parsch
|
|
.
Discoverer 75 / CORONA
1006 / KH-4A
Spacecraft: |
OPS 3483 |
Chronologies: |
1964 payload #52 ; 1964-027A ; 394th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Kosmos 31
Spacecraft: |
DS-MT No. 2 |
Chronologies: |
1964 payload #43 ; 1964-028A ; 395th spacecraft. |
Type: |
Earth/space studies (civil) |
Spnsor: |
Soviet Union |
|
|
|
.
Kosmos 32
Spacecraft: |
Zenit-2 No. 18 |
Chronologies: |
1964 payload #44 ; 1964-029A ; 396th spacecraft. |
Type: |
Reconnaisance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Discoverer 76 / CORONA
9063A / KH-5
Spacecraft: |
OPS 3236 |
Chronologies: |
1964 payload #45 ; 1964-030A ; 397th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Starflash 1A
Spacecraft: |
|
Chronologies: |
1964 payload #46 ; 1964-030A ; 398th spacecraft. |
Type: |
Technology? |
Sponsor: |
U.S. Air Force |
|
|
|
.
P-35-8 / DAPP 8
Spacecraft: |
OPS 4467A ; AFP-43
Data Acquisition and Processing Program |
Chronologies: |
1964 payload #47 ; 1964-031A ; 399th spacecraft. |
Type: |
Technology |
Sponsor: |
U.S. Air Force |
|
|
|
.
P-35-9 / DAPP 9
Spacecraft: |
OPS 4467B ; AFP-43
Data Acquisition and Processing Program |
Chronologies: |
1964 payload #48 ; 1964-031C ; 400th spacecraft. |
Type: |
Technology |
Sponsor: |
U.S. Air Force |
|
|
|
.
Discoverer 77 / CORONA
1007 / KH-4A
Spacecraft: |
OPS 3754 ; |
Chronologies: |
1964 payload #49 ; 1964-032A ; 401st spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Kosmos 33
Spacecraft: |
Zenit-2 No. 20 |
Chronologies: |
1964 payload #50 ; 1964-033A ; 402nd spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
ESRS / AFCRL B
Spacecraft: |
Environmental Sciences Research
Satellite |
Chronologies: |
1964 payload #51 ; 1964 10th loss ; 403rd
spacecraft. |
Type: |
Earth upper atmosphere studies |
Sponsor: |
U.S. Air Force |
|
|
Launch: |
25 June 1964 at 1h40 UTC, from
Vandenberg Air Force Base's LC-D, by a Scout (X-4 S128R). |
Orbit: |
|
Decayed: |
|
Mission: |
Although details
remain sketchy, it appears as if an experimental radar satellite program
was started during the Kennedy administration. This program, known as Quill,
produced three satellites: two flight models and a test model. One satellite
was launched in 1964. It used a radar that was probably built by Raytheon
to take images of the ground which were stored on magnetic tape. Quill
used the same recovery system as the Corona reconnaissance satellite, returning
the magnetic tape to Earth in a recoverable capsule that was caught in
mid-air by an aircraft.
Apparently, the
flight and the mission were successful, but the program was not continued.
It is easy to speculate why. The satellite’s relatively low power and early
technology undoubtedly limited its capabilities, particularly the size
of objects it could spot. Quill could probably not spot anything smaller
than a naval vessel. In addition, the data retrieval technique meant that
information was not processed until long after it had been collected. The
intelligence value was therefore probably too limited to justify further
efforts. |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's ENSAT
; TRW Space Log ; Space Review's 22
Jan 07 ; |
|
|
.
AC-3 / Atlas-Centaur
3
Spacecraft: |
Centaur 1C |
Chronologies: |
1964 payload #52 ; 1964 11th loss ; 404th
spacecraft. |
Type: |
Technology |
Sponsor: |
NASA |
|
|
|
.
Kosmos 34
Spacecraft: |
Zenit-4 |
Chronologies: |
1964 payload #53 ; 1964-034A ; 405th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Ferret 6
Spacecraft: |
OPS 3395 |
Chronologies: |
1964 payload #54 ; 1964-035A ; 406th spacecraft. |
Type: |
Electronic intelligence |
Sponsor: |
U.S. Air Force |
|
|
|
.
Improve Samos 9 / KH-7
9
Spacecraft: |
OPS 3684 ; AFP-206 SV 959 |
Chronologies: |
1964 payload #55 ; 1964-036A ; 407th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Hitchhiker 5
Spacecraft: |
OPS 4923 / [EHH A3] |
Chronologies: |
1964 payload #56 ; 1964-036B ; 408th spacecraft. |
Type: |
Electronic intelligence |
Sponsor: |
U.S. Air Force |
|
|
Launch: |
6 July 1964 at 18h51 UTC, from
Vandenberg Air Force Base (Point Arguello)'s LC-2-3, by an Atlas-Agena
D (Atlas LV-3A 352D / Agena D S01A 4807).. |
Orbit: |
|
Decayed: |
|
Mission: |
|
Note: |
“Reported in Astronuutics and Aerospace
Engineering that a 'hitchhiker' satellite called Satar (Satellite-Aerospace
Research) would be built and tested by General Dynamics. A bullet-shaped
spacecraft 3.7-metre long and 75 cm in diameter, Satar would be incorporated
in Atlas missiles used for training missions. It would consist of a payload
section capable of accommodating “several hundred pounds of experiments”
and a propulsion section including a solid-propellant motor, guidance,
attitude control, and related equipment. Satar would be released after
Atlas burnout and about 15 min. before its own engine ignited to send it
into orbit. First flight was scheduled for next spring.” (A&A
1963, p. 455) |
Source: |
Jonathan
McDowell's
Master
List ; Mark
Wade’s Encyclopedia Astronautica ; National
Space Science Data Center's 1964-036B
; TRW Space Log ; |
|
|
.
Elektron 3
Spacecraft: |
2D No. 3 |
Chronologies: |
1964 payload #57 ; 1964-038A ; 409th spacecraft. |
Type: |
Earth upper atmosphere and radiations studies |
Sponsor: |
Soviet Union |
|
|
|
.
Elektron 4
Spacecraft: |
2D No. 4 |
Chronologies: |
1964 payload #59 ; 1964-038B ; 410th spacecraft. |
Type: |
Earth upper atmosphere and radiations studies |
Sponsor: |
Soviet Union |
|
|
|
.
Discoverer 78 / CORONA
1008 / KH-4A
Spacecraft: |
OPS 3491 |
Chronologies: |
1964 payload #59 ; 1964-037A ; 411th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Kosmos 35
Spacecraft: |
Zenit-2 No. 21 |
Chronologies: |
1964 payload #60 ; 1964-039A ; 412th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Vela Hotel 3 / Vela
2A
Spacecraft: |
|
Chronologies: |
1964 payload #61 ; 1964-040A ; 413th spacecraft. |
Type: |
Nuclear explosion monitoring |
Sponsor: |
U.S. Air Force |
|
|
|
.
Vela Hotel 4 / Vela
2B
Spacecraft: |
|
Chronologies: |
1964 payload #62 ; 1964-040B ; 414th spacecraft. |
Type: |
Nuclear explosion monitoring |
Sponsor: |
U.S. Air Force |
|
|
|
.
ERS 13 / TRS 6
Spacecraft: |
TRS 2(B) |
Chronologies: |
1964 payload #63 ; 1964-040C ; 415th spacecraft. |
Type: |
Technology |
Sponsor: |
U.S. Air Force |
|
|
|
.
Ranger 7
Spacecraft: |
|
Chronologies: |
1964 payload #64 ; 1964-041A ; 416th spacecraft. |
Type: |
Lunar probe |
Sponsor: |
NASA |
|
|
|
.
Kosmos 36
Spacecraft: |
DS-P1-Yu No. 1 |
Chronologies: |
1964 payload #65 ; 1964-042A ; 417th spacecraft. |
Type: |
Military technologies |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Discoverer 79 / CORONA
1009 / KH-4A
Spacecraft: |
OPS 3042 |
Chronologies: |
1964 payload #66 ; 1964-043A ; 418th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Kosmos 37
Spacecraft: |
Zenit-2 No. 22 |
Chronologies: |
1964 payload #67 ; 1964-044A ; 419th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Improve Samos 10 / KH-7
10
Spacecraft: |
OPS 3802 ; AFP-206 SV 960 |
Chronologies: |
1964 payload #68 ; 1964-045A ; 420th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Hitchhiker 6
Spacecraft: |
OPS 3316 / P-11 No. 4202 |
Chronologies: |
1964 payload #69 ; 1964-045B ; 421st spacecraft. |
Type: |
Electronic intelligence |
Sponsor: |
U.S. Air Force |
|
|
|
.
Kosmos 38
Spacecraft: |
Strela-1 |
Chronologies: |
1964 payload #70 ; 1964-046A ; 422nd spacecraft. |
Type: |
Communications (store-dump) |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Kosmos 39
Spacecraft: |
Strela-1 |
Chronologies: |
1964 payload #71 ; 1964-046B ; 423rd spacecraft. |
Type: |
Communications (store-dump) |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Kosmos 40
Spacecraft: |
Strela-1 |
Chronologies: |
1964 payload #72 ; 1964-046C ; 424th spacecraft. |
Type: |
Communications (store-dump) |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Syncom 3
Spacecraft: |
Syncom C |
Chronologies: |
1964 payload #73 ; 1964-047A ; 425th spacecraft. |
Type: |
Communications |
Sponsor: |
NASA |
|
|
|
.
Discoverer 80 / CORONA
9064A / KH-5
Spacecraft: |
OPS 2739 |
Chronologies: |
1964 payload #74 ; 1964-048A ; 426th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Starflash 1B
Spacecraft: |
|
Chronologies: |
1964 payload #75 ; 1964-048B ; 427th spacecraft. |
Type: |
Technology? |
Sponsor: |
U.S. Air Force |
|
|
|
.
Kosmos 41
Spacecraft: |
Molniya-1 |
Chronologies: |
1964 payload #76 ; 1964-049A ; 428th spacecraft. |
Type: |
Communications |
Sponsor: |
Soviet Union |
|
|
|
.
Kosmos 42
Spacecraft: |
Strela-1 |
Chronologies: |
1964 payload #77 ; 1964-050A ; 429th spacecraft. |
Type: |
Communications (store/dump) |
Sponsor: |
Soviet Union Defense ministry |
|
|
|
.
Kosmos 43
Spacecraft: |
Strela-1 |
Chronologies: |
1964 payload #78 ; 1964-050B ; 430th spacecraft. |
Type: |
Communications (store/dump) |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Explorer 20 / IE-A /
TOPSI
Spacecraft: |
NASA S-48 |
Chronologies: |
1964 payload #79 ; 1964-051A ; 431st spacecraft. |
Type: |
Earth upper atmosphere studies |
Sponsor: |
NASA |
|
|
|
.
Nimbus 1
Spacecraft: |
Nimbus A |
Chronologies: |
1964 payload #80 ; 1964-052A ; 432nd spacecraft. |
Type: |
Meteorology |
Sponsor: |
NASA |
|
|
|
.
Kosmos 44
Spacecraft: |
Meteor No. 1 |
Chronologies: |
1964 payload #81 ; 1964-053A ; 433rd spacecraft. |
Type: |
Meteorology |
Sponsor: |
Soviet Union |
|
|
|
.
Transtage
Spacecraft: |
Transtage 2 |
Chronologies: |
1964 payload #82 ; 1964 12th loss ; 434th
spacecraft. |
Type: |
Technology |
Sponsor: |
U.S. Air Force |
|
|
|
.
OGO 1 / EOGO 1
Spacecraft: |
OGO A / Orbiting Geophysical
Observatories |
Chronologies: |
1964 payload #83 ; 1964-054A ; 435th spacecraft. |
Type: |
Geophysics |
Sponsor: |
NASA |
|
|
|
.
Kosmos 45
Spacecraft: |
Zenit-4 |
Chronologies: |
1964 payload #84 ; 1964-055A ; 436th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Discoverer 81 / CORONA
1010 / KH-4A
Spacecraft: |
OPS 3497 |
Chronologies: |
1964 payload #85 ; 1964-056A ; 437th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Apollo SA-7
Spacecraft: |
Apollo BP-15 |
Chronologies: |
1964 payload #86 ; 1964-057A ; 438th spacecraft. |
Type: |
Piloted spacecraft test |
Sponsor: |
NASA |
|
|
|
.
Improve Samos 11 / KH-7
11
Spacecraft: |
OPS 4262 ; AFP-206 SV 962 |
Chronologies: |
1964 payload #87 ; 1964-058A ; 439th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Kosmos 46
Spacecraft: |
Zenit-2 No. 23 |
Chronologies: |
1964 payload #88 ; 1964-059A ; 440th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Explorer 21 / IMP 2
Spacecraft: |
IMP B |
Chronologies: |
1964 payload #89 ; 1964-060A ; 441st spacecraft. |
Type: |
Earth-space studies |
Sponsor: |
NASA |
|
|
|
.
Discoverer 82 / CORONA
1011 / KH-4A
Spacecraft: |
OPS 3333 |
Chronologies: |
1964 payload #90 ; 1964-061A ; 442nd spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Kosmos 47
Spacecraft: |
Voskhod 3KV No. 2 |
Chronologies: |
1964 payload #91 ; 1964-062A ; 443rd spacecraft. |
Type: |
Piloted spacecraft test |
Sponsor: |
Soviet Union (Korolev's Design Bureau) |
|
|
|
.
Transit O-1
Spacecraft: |
Transit 5B-4 / NNS O-1 / NNS
30010 |
Chronologies: |
1964 payload #92 ; 1964-063A ; 444th spacecraft. |
Type: |
Navigation |
Sponsor: |
U.S. Navy |
|
Source: A.
Parsch
|
|
.
Calsphere 1 / Dragsphere
1
Spacecraft: |
|
Chronologies: |
1964 payload #93 ; 1964-063B ; 445th spacecraft. |
Type: |
Radar calibration |
Sponsor: |
U.S. Air Force & U.S. Navy |
|
|
|
.
Calsphere 2 / Dragsphere
2
Spacecraft: |
|
Chronologies: |
1964 payload #94 ; 1964-063C ; 446th spacecraft. |
Type: |
Radar calibration |
Sponsor: |
U.S. Air Force & U.S. Navy |
|
|
|
.
Improve Samos 12 / KH-7
12
Spacecraft: |
OPS 4036 ; AFP-206 SV 961 |
Chronologies: |
1964 payload #95 ; 1964 13th loss ; 447th
spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Explorer 22 / BE-B
Spacecraft: |
Beacon Explorer B |
Chronologies: |
1964 payload #96 ; 1964-064A ; 448th spacecraft. |
Type: |
Earth upper atomphere studies |
Sponsor: |
NASA |
|
|
|
.
Voskhod
Spacecraft: |
Voskhod 3KV No. 3 |
Chronologies: |
1964 payload #97 ; 1964-065A ; 449th spacecraft. |
Type: |
Piloted spacecraft |
Sponsor: |
Soviet Union (Korolev's Design Bureau) |
|
|
|
.
Kosmos 48
Spacecraft: |
Zenit-2 No. 24 |
Chronologies: |
1964 payload #98 ; 1964-066A ; 450th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. Air Force |
|
|
|
.
Discoverer 83 / CORONA
1012 / KH-4A
Spacecraft: |
OPS 3559 |
Chronologies: |
1964 payload #99 ; 1964-067A ; 451st spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Kosmos
Spacecraft: |
Strela-1 |
Chronologies: |
1964 payload #100 ; 1964 14th loss ; 452nd
spacecraft. |
Type: |
Communications (store/dump) |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Kosmos
Spacecraft: |
Strela-1 |
Chronologies: |
1964 payload #101 ; 1964 15th loss ; 453rd
spacecraft. |
Type: |
Communications (store/dump) |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Kosmos
Spacecraft: |
Strela-1 |
Chronologies: |
1964 payload #102 ; 1964 16th loss ; 454th
spacecraft. |
Type: |
Communications (store/dump) |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Improve Samos 13 / KH-7
13
Spacecraft: |
OPS 4384 ; AFP-206 SV 963 |
Chronologies: |
1964 payload #103 ; 1964-068A ; 455th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Hitchicker 7
Spacecraft: |
OPS 5063 / [EHH A4] |
Chronologies: |
1964 payload #104 ; 1964-068B ; 456th spacecraft. |
Type: |
Electtronic intelligence |
Sponsor: |
U.S. Air Force |
|
|
|
.
Kosmos 49
Spacecraft: |
DS-MG No. 2 |
Chronologies: |
1964 payload #105 ; 1964-069A ; 457th spacecraft. |
Type: |
Military technologies |
Sponsor: |
Soviet Union |
|
|
|
.
Kosmos 50
Spacecraft: |
Zenit-2 No. 25 |
Chronologies: |
1964 payload #106 ; 1964-070A ; 458th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Discoverer 84 / CORONA
1013 / KH-4A
Spacecraft: |
OPS 5434 |
Chronologies: |
1964 payload #107 ; 1964-071A ; 459th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Ferret 7
Spacecraft: |
OPS 3062 |
Chronologies: |
1964 payload #108 ; 1964-072A ; 460th spacecraft. |
Type: |
Electronic intelligence |
Sponsor: |
U.S. Air Force |
|
|
|
.
Mariner 3
Spacecraft: |
Mariner C-2, |
Chronologies: |
1964 payload #109 ; 1964-073A ; 461st spacecraft. |
Type: |
Mars probe |
Sponsor: |
NASA |
|
|
|
.
Explorer 23
Spacecraft: |
NASA S-55C |
Chronologies: |
1964 payload #110 ; 1964-074A ; 462nd spacecraft. |
Type: |
Micrometeroids studies |
Sponsor: |
NASA |
|
|
|
.
Discoverer 85 / CORONA
1014 / KH-4A
Spacecraft: |
OPS 3360 |
Chronologies: |
1964 payload #111 ; 1964-075A ; 463rd spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
ORBIS
Spacecraft: |
|
Chronologies: |
1964 payload #112 ; 1964-075B ; 464th spacecraft. |
Type: |
Technology? |
Sponsor: |
U.S. Air Force? |
|
|
|
.
Explorer 24 / AD-B
Spacecraft: |
Air Density |
Chronologies: |
1964 payload #113 ; 1964-076A ; 465th spacecraft. |
Type: |
Earth upper atmospheric studies |
Sponsor: |
NASA |
|
|
|
.
Explorer 25 / Injun
4
Spacecraft: |
|
Chronologies: |
1964 payload #114 ; 1964-076B ; 466th spacecraft. |
Type: |
Energetic particles studies |
Sponsor: |
NASA |
|
|
|
.
Mariner 4
Spacecraft: |
Mariner C-3 |
Chronologies: |
1964 payload #115 ; 1964-077A ; 467th spacecraft. |
Type: |
Mars probe |
Sponsor: |
NASA |
|
|
|
.
Zond 2
Spacecraft: |
3MV-4A No. 2 |
Chronologies: |
1964 payload #116 ; 1964-078A ; 468th spacecraft. |
Type: |
Mars probe |
Sponsor: |
Soviet Union (Korolev's Design Bureau) |
|
|
|
.
Kosmos
Spacecraft: |
DS-2 No. 2 |
Chronologies: |
1964 payload #117 ; 1964 17th loss ; 469th
spacecraft. |
Type: |
Technology and Earth upper atmosphere studies |
Sponsor: |
Soviet Union's Defense ministry |
|
|
|
.
Improve Samos 14 / KH-7
14
Spacecraft: |
OPS 4439 ; AFP-206 SV 964 |
Chronologies: |
1964 payload #118 ; 1964-079A ; 470th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
|
|
.
Kosmos 51
Spacecraft: |
DS-MT No. 3 |
Chronologies: |
1964 payload #119 ; 1964-080A ; 471st spacecraft. |
Type: |
Earth/space studies (civil) |
Sponsor: |
Soviet Union |
|
|
|
.
Transtage 1
Spacecraft: |
Transtage 2 |
Chronologies: |
1964 payload #120 ; 1964-081A ; 472nd spacecraft. |
Type: |
Technology |
Sponsor: |
U.S. Air Force |
|
|
|
.
Surveyor SD-1 (AC-4)
Spacecraft: |
Centaur 4C |
Chronologies: |
1964 payload #121 ; 1964-082A ; 473rd spacecraft. |
Type: |
Technology |
Sponsor: |
NASA |
|
|
|
.
Transit 5E5
Spacecraft: |
Transit VE-5 / APL SN-43 |
Chronologies: |
1964 payload #122 ; 1964-083A ; 474th spacecraft. |
Type: |
Navigation |
Sponsor: |
U.S. Navy/U.S. Air Force |
|
|
|
.
Transit O-2 / NNS O-2
Spacecraft: |
|
Chronologies: |
1964 payload #123 ; 1964-083B ; 475th spacecraft. |
Type: |
Navigation |
Sponsor: |
U.S. Navy/U.S Air Force |
|
|
|
.
San Marco 1
Spacecraft: |
|
Chronologies: |
1964 payload #124 ; 1964-084A ; 476th spacecraft. |
Type: |
Earth upper atmosphere studies |
Sponsor: |
Italy |
|
|
|
.
Discoverer 86 / CORONA
1015 / KH-4A
Spacecraft: |
OPS 3358 |
Chronologies: |
1964 payload #125 ; 1964-085A ; 477th spacecraft. |
Type: |
Reconnaissance |
Sponsor: |
U.S. National Reconnaissance Office |
|
 |
|
.
Explorer 26 / EPE-D
Spacecraft: |
|
Chronologies: |
1964 payload #126 ; 1964-086A ; 478th spacecraft. |
Type: |
Particles and geomagnetic field studies |
Sponsor: |
NASA |
|
|
|
.
QUILL / Ferret 11
Spacecraft: |
OPS 3762 / FTV 2355 |
Chronologies: |
1964 payload #127 ; 1964-087A ; 479th spacecraft. |
Type: |
Electronic intelligence |
Sponsor: |
U.S. Air Force |
|
|
Launch: |
21 December 1964 at 19h08 UTC,
from Vandenberg Air Force Base's LC-75-1-1, by a Thor-Agena D (Thor 2C
425 / Agena D SS-01A 2355). |
Orbit: |
236 km x 263 km x 70.1° |
De-orbited: |
11 January 1965 at 10h27 UT (capsule recovered
on 23 December 1964 at 20h56 UT) |
Mission: |
QUILL was the world's first SAR (synthetic
aperture radar) imaging satellite, flown as a proof of concept and used
to image test targets in the U.S., proving that space radar could identify
features through cloud cover. The 1,477-kg satellite consisted of a modified
CORONA/Agena vehicle, with a 0.6 x 4.6-metre X-band radar antenna panel
flush with the body of the Agena D upper stage. The camera system in the
payload body was replaced by the KP-II radar itself and a recorder/transmitter
system. The 139-kg SRV CORONA-type recovery capsule was recovered
on 23 December 1964 in mid-air over the Pacific, northeast of Hawaii. The
KP-II radar continued operations until 26 December, when the spacecraft
batteries failed, and the QUILL spacecraft reentered on 11 January 1965
over the South Atlantic. |
Source: |
Jonathan
McDowell's
Master
List & 662
; Mark Wade’s
Encyclopedia Astronautica ; National
Space Science Data Center's 1964-087A
; TRW Space Log ; |
|
|
|