1966 Launcher and Payload
Scoreboard |
Soviet Launches |
American Launches |
|
Launcher |
S/F |
Payload |
Mass orbited |
38 |
A / 'Vostok' |
S |
Kosmos
104 / Zenit-2 |
4,700 kg |
|
|
S |
Kosmos
105 / Zenit-2 |
4,720 kg |
|
|
S |
Luna
9 |
1,580 kg |
|
|
S |
Kosmos
107 / Zenit-2 |
4,720 kg |
|
|
S |
Kosmos
109 / Zenit-4 |
6,300 kg |
|
|
S |
Kosmos
110/Voskhod |
5,700 kg |
|
|
F* |
Kosmos
111 / E-6S |
6,541 kg |
|
|
S |
Kosmos
112 / Zenit-2 |
4,720 kg |
|
|
S |
Kosmos
113 / Zenit-4 |
6,300 kg |
|
|
F |
Molniya |
(1,600 kg) |
|
|
S |
Luna
10 |
1,597 kg |
|
|
S |
Kosmos
114 / Zenit-4 |
6,300 kg |
|
|
S |
Kosmos
115 / Zenit-2 |
4,720 kg |
|
|
S |
Molniya
1-3 |
4,600 kg |
|
|
S |
Kosmos
117 / Zenit-2 |
4,720 kg |
|
|
S |
Kosmos
118 / Meteor |
4,730 kg |
|
|
F |
Kosmos
/ Zenit-4 |
(unknown) |
|
|
S |
Kosmos
120 / Zenit-2 |
4,720 kg |
|
|
S |
Kosmos
121 / Zenit-4 |
6,300 kg |
|
|
S |
Kosmos
122 / Meteor |
4,730 kg |
|
|
S |
Kosmos
124 / Zenit-2 |
4,720 kg |
|
|
S |
Kosmos
125 / US-A |
3,800 kg |
|
|
S |
Kosmos
126 / Zenit-4 |
6,300 kg |
|
|
S |
Kosmos
127 / Zenit-4 |
6,300 kg |
|
|
S |
Luna
11 |
1,638 kg |
|
|
S |
Kosmos
128 / Zenit-4 |
6,300 kg |
|
|
F |
Kosmos
/ Zenit-2 |
(4,720 kg) |
|
|
S |
Kosmos
129 / Zenit-2 |
4,720 kg |
|
|
S |
Molniya
1-4 |
1,600 kg |
|
|
S |
Kosmos
130 / Zenit-4 |
6.300 kg |
|
|
S |
Luna
12 |
1,620 kg |
|
|
S |
Kosmos
131 / Zenit-4 |
6,300 kg |
|
|
S |
Kosmos
132 / Zenit-2 |
4,720 kg |
|
|
S |
Kosmos
133 / Soyuz |
6,450 kg |
|
|
S |
Kosmos
134 / Zenit-4 |
6,300 kg |
|
|
F |
Kosmos
/ Soyuz 1 |
(unknonw) |
|
|
S |
Kosmos
136 / Zenit-2 |
4,700 kg |
|
|
S |
Luna
13 |
1,700 kg |
8 |
B / Kosmos |
S |
Kosmos
106 / DS-P1 |
325 kg |
|
|
S |
Kosmos
108 / DS-U1- |
255 kg |
|
|
F |
Kosmos
/ DS-K-40 2 |
(unknown) |
|
|
S |
Kosmos
116 / DS-P1- |
325 kg |
|
|
S |
Kosmos
119 / DS-U2- |
250 kg |
|
|
S |
Kosmos
123 / DS-P1- |
325 kg |
|
|
S |
Kosmos
135 / DS-U2- |
355 kg |
|
|
S |
Kosmos
137 / DS-U2- |
295 kg |
5 |
R-36 |
S |
OGCh
02L |
(1,700 kg*) |
|
|
S |
OGCh
03L |
(1,700 kg*) |
|
|
? |
OGCh
No. 04L |
(1,700 kg*) |
|
|
S |
OGCh |
1,700 kg |
|
|
S |
OGCh |
1,700 kg |
2 |
D / Proton |
F |
Proton |
(8,300 kg) |
|
|
S |
Proton
3 |
8,300 kg |
1 |
C / Kosmos |
F |
Kosmos
/ Strela |
(unknown) |
.* The first three FOBS
tests are sub-orbital flight, so not counted in mass orbited.
.
Keys: |
F = launch failure
F* = the rocket failed but its had placed
its payload into (low) Earth orbit.
S = launch success
brakets () = mass not counted |
|
|
Launcher |
S/F |
Payload |
Mass orbited |
33 |
Atlas |
S |
KH-7
24,
Agena
Pickaback |
2,000 kg
60 kg |
|
|
S |
KH-7
25,
Bluebell
2C,
Bluebell
2S |
2,000 kg
9 kg
4 kg |
|
|
S |
GATV
8 / TDA 3 |
3,175 kg |
|
|
S |
KH-7
26,
Agena
Pickaback |
2,000 kg
60 kg |
|
|
S |
A-302
/ SPP 28,
OV
1-4,
OV
1-5 |
unknown
88 kg
114 kg |
|
|
S |
Surveyor
Model 3 |
784 kg |
|
|
S |
OAO
1 |
1,774 kg |
|
|
S |
KH-7
27 |
2,000 kg |
|
|
S |
KH-7
28,
Hitchhiker
11 |
2,000 kg
60 kg |
|
|
F |
GATV
9 / TDA 5 |
(3,248 kg) |
|
|
S |
Surveyor
1 |
269 kg |
|
|
S |
ATDA
/ TDA 4 |
794 kg |
|
|
S |
KH-7
29,
Agena
Pickaback |
2,000 kg
60 kg |
|
|
S |
OGO
3 / EOGO 3 |
634 kg |
|
|
F |
Midas
10 ,
Secor
6 / EGRS 6,
ERS
16 / ORS 2 |
2,000 kg
17 kg
15 kg |
|
|
S |
KH-7
30 |
2,200 kg |
|
|
S |
OV
1-8,
OV
1-7,
OV
1-subsat |
unknown
10 kg
unknown |
|
|
S |
GATV
10 / TDA 1A |
1,175 kg |
|
|
S |
Lunar
Orbiter 1 |
386 kg |
|
|
S |
KH-7
31,
Hitchhiker
12 |
2,000 kg
60 kg |
|
|
S |
Midas
11,
Secor
7 / EGRS 7,
ERS
15 / ORS 1 |
2,000 kg
17 kg
5 kg |
|
|
S |
GATV
11 / TDA 6 |
3,175 kg |
|
|
S |
KH-7
32,
Hitchhiker
13 |
2,000 kg
60 kg |
|
|
S |
Surveyor
2 |
272 kg |
|
|
S |
Midas
12,
Secor
8 / EGRS 8 |
2,000 kg
17 kg |
|
|
S |
KH-7
33,
SGLS
1 |
2,000 kg
60 kg |
|
|
S |
Surveyor
Model 4 |
951 kg |
|
|
S |
KH-7
34,
Agena
Pickaback |
2,000 kg
60 kg |
|
|
S |
Lunar
Orbiter 2 |
390 kg |
|
|
S |
GATV
12 / TDA 7 |
3,175 kg |
|
|
S |
KH-7
35 |
2,000 kg |
|
|
S |
ATS
1 |
352 kg |
|
|
S |
OV
1-9,
OV
1-10 |
230 kg
130 kg |
16 |
Thor |
S |
P-35-14
/ DAPP 14 |
130 kg |
|
|
S |
Discoverer
100 / KH-4A |
1,500 kg |
|
|
S |
Ferret
9 |
1,500 kg |
|
|
S |
Discoverer
101 / KH-4A |
1,500 kg |
|
|
S |
P-35-15
/ DAPP 15 |
130 kg |
|
|
S |
Discoverer
102 / KH-4A |
1,500 kg |
|
|
F |
Discoverer
103 / KH-4A |
(1,500 kg) |
|
|
S |
Nimbus
3 |
414 kg |
|
|
S |
Discoverer
104 / KH-4A |
1,500 kg |
|
|
S |
Discoverer
105 / KH-4A |
1,500 kg |
|
|
S |
Pageos
A |
55 kg |
|
|
S |
Discoverer
106 / KH-4A |
1,500 kg |
|
|
S |
P-35-16 |
125 kg |
|
|
S |
Discoverer
107 / KH-4A |
1,500 kg |
|
|
S |
Discoverer
108 / KH-4A |
1,500 kg |
|
|
S |
Ferret
10 |
1,500 kg |
11 |
Titan |
S |
Gemini
VIII |
3,788 kg |
|
|
S |
Gemini
IX-A |
3,668 kg |
|
|
S |
GGTS
1,
IDSCP
1-1,
IDSCP
1-2,
IDSCP
1-3,
IDSCP
1-4,
IDSCP
1-5,
IDSCP
1-6,
IDSCP
1-7 |
47 kg
45 kg
45 kg
45 kg
45 kg
45 kg
45 kg
45 kg |
|
|
S |
Gemini
X |
3.763 kg |
|
|
S |
KH-8
1 GAMBIT |
2,000 kg |
|
|
F |
IDCSP
8,
IDCSP
9,
IDCSP
10,
IDCSP
11,
IDCSP
12,
IDCSP
13,
IDCSP
14,
IDCSP
15 |
(45 kg)
(45 kg)
(45 kg)
(45 kg)
(45 kg)
(45 kg)
(45 kg)
(45 kg) |
|
|
S |
Gemini
XI |
3,798 kg |
|
|
S |
KH-8
2 GAMBIT |
2,000 kg |
|
|
S |
OV
4-3,
MOL
/ Gemini B,
OV
4-1R,
OV
4-6S,
OV
4-1T |
9,680 kg
1,800 kg
unknown
202 kg
109 kg |
|
|
S |
Gemini
XII |
3,763 kg |
|
|
S |
KH-8
3 GAMBIT |
2,000 kg |
8 |
Delta |
S |
ESSA
1 |
138 kg |
|
|
S |
ESSA-2 |
132 kg |
|
|
S |
Explorer
32 |
225 kg |
|
|
S |
Explorer
33 |
93 kg |
|
|
S |
Pioneer
7 |
63 kg |
|
|
S |
ESSA
3 |
145 kg |
|
|
S |
Intelsat
2A |
140 kg |
|
|
S |
Biosatellite
1 |
425 kg |
8 |
Scout |
S |
Transit
11 |
50 kg |
|
|
S |
Transit
12 |
50 kg |
|
|
S |
OV
3-1 |
69 kg |
|
|
S |
Transit
13 |
50 kg |
|
|
S |
OV
3-4 |
79 kg |
|
|
S |
OV
3-3 |
75 kg |
|
|
S |
Transit
14 |
58 kg |
|
|
S |
OV
3-2 |
82 kg |
3 |
Saturn |
S |
Apollo
AS-201 |
(20,820 kg*) |
|
|
S |
Apollo
2 / AS-203 |
26,500 kg |
|
|
S |
Apollo
AS-202 |
25,809 kg |
* Apollo AS-201 was a sub-orital mission, thus
not counted as mass orbite |
1966 Summary: |
|
48 launch successes in 54 tries (85% success)
175 tons orbited |
75 launch successes in 79 tries (95% success)
154 tons orbited |
1957-1966 Summary: |
|
116 launch successes in 220 tries (76% success)
535 tons orbited |
354 launch successes in 440 tries (81% success)
515 tons orbited |
|