| |
 |
| A4 |
|
 |
A4 |
|
| |
Engines:
1. 1 × Model 39
Total mass: 12,800 kg
Apogee: 85 km
First launch: 1946 |
 |
Hermes B1
Engines:
1. 1 × Model 39
First launch: 1947 |
|
Bumper
Engines:
1. 1 × Model 39
2. 1 × WAC-Corporal
Total mass: 12,862 kg
Apogee: 250 km
First launch: 1948 |
 |
Launches: 76 (Failures: 30)
/1946-1952/
(Ā4)
(Hermes)
(Bumper)
|
L
64
4
8
|
F
24
1
5
|
/1946-1952/
/1947-1950/
/1948-1950/ |
|
 |
Retired |
|
| WAC A-0 |
|
|
WAC A, B |
|
| |
(WAC-Corporal)
Engines:
1. 1 × Tiny Tim
2. 1 × WAC-Corporal
Total mass: 300 kg
Apogee: 75 km
First launch: 1945
|
|
Launches: 30 (Failures: 3)
/1945-1947/
(WAC A-0)
(WAC A)
(WAC B)
|
L
13
14
8
|
F
3
|
/1945-1946/
/1945-1946/
/1946-1947/ |
|
|
Retired |
|
|
| Aerobee |
 |
|
|
|
|
|
|
|
|
| Aerobee |
 |
|
|
|
|
|
|
|
|
Aerobee-100
Engines:
1. 1 × AJ × 103C10
2. 1 × Aerobee-100 |
|
Aerobee-Hi / 150 / 300
Engines:
1. 1 × AJ × 103C10
2. 1 × Aerobee-150
3. 1 × Sparrow (300) |
|
Aerobee-170 / 200
Engines:
1. 1 × Nike | M5-E1
2. 1 × Aerobee-150 (170)
1 × Aearobee AJ10-91 (200) |
|
Aerobee-350
Engines:
1. 1 × Nike | M5-E1
2. 4 × Aerobee AJ10-91
|
| Total mass: |
700 kg
930 / 1,270 kg
983 / 1,600 kg
3,839 kg |
(100)
(150 / 170)
(300 / 200)
(350) |
| |
| Apogee: |
100 km
270 / 220 km
300 / 250 km
450 km |
(100)
(150 / 170)
(300 / 200)
(350) |
|
|
Launches: 1051 (Failures: 68)
/1947-1985/
|
|
Retired |
|
|
|
| Pilot / NOTS |
 |
|
|
|
 |
Pilot / NOTS
Engines:
0. F-4D1 (aircraft)
1. 2 × HOTROC
2. 2 × HOTROC
3. 1 × ABL × -241
4. 1 × NOTS-100
5. 1 × NOTS |
|
Launches: 10 (Failures: 10)
/1958/
|
|
Retired |
|
|
| Caleb / NOTS |
|
|
|
|
|
|
|
Caleb / NOTS
Engines:
0. F-4D1 (aircraft)
1. 1 × NOTS-500
2. 1 × X-248
3. 1 × NOTS-100A
4. 1 × NOTS-300 |
|
Launches: 7 (Failures: 2)
/1960-1962/
|
|
Retired |
|
|
|
| Pedro Recruit |
|
|
|
|
|
Pedro Recruit
Engines:
0. F-4 (aircraft)
1. 1 × Pedro
2. 1 × Recruit
Apogee: 20 km |
|
Launches: 8 (Failures: 0)
/1975-1976/
|
|
| |
|
Sergeant
Engines:
1. 1 × Sergeant | TX-20
Total mass: 4,530 kg
Apogee: 80 km
Maximum range: 139 km
Warhead: 820 kg / 200 KT
First launch: 1956
Operational Capability: 1962 |
|
|
|
|
| X-17A |
|
|
|
|
|
X-17A (Pegasus )
Engines:
1. 1 × Sergeant | TX-20
2. 3 × Recruit | XM-19
3. 1 × Recruit | XM-19
Total mass: 3,400 kg
Apogee: 500 km |
|
Launches: 39 (Failures: 9)
/1955-1958/
|
Payload: reentry, Argus (Nuke) |
|
|
|
|
|
|
| Blue Scout Jr |
|
|
|
|
|
Blue Scout Junior
Engines:
1. 1 × Castor-1 | XM-33E8
2. 1 × Antares-1A | × -254-A1
3. none
1 × Alcor | AJ10-41
1 × Altair | × -248
4. none
1 × Cetus | NOTS-100A |
|
Launches: 25 (Failures: 6)
/1960-1970/
|
|
|
|
Strypi
Engines:
0. 2 × Recruit | XM-19
1. 1 × Castor-1 | XM-33E8
2. 1 × Star-26 (4, 4R)
1 × Alcor (7R)
1 × Antares-2A (9, 11)
3. 1 × Alcyone | BE-3 (7R)
1 × Star-27 (11)
Total mass: 5,500 kg (2)
| |
| Apogee: |
208 km
250 km
500 km
|
(2R)
(2AR)
(4) |
|
200 km
200 km
120 km |
(6)
(7, 9)
(11) |
|
|
Launches:
(2)
(4)
(6)
(7)
(9)
(11) |
3
3
3
4
2
4 |
/1974-1979/
/1966-1976/
/1968-1970/
/1972-1975/
/1995/
/1987-1991/ |
|
|
Astrobee-1500
Engines:
0. 2 × Recruit | XM-19
1. 1 × Aerojet Junior
2. 1 × Alcor
Total mass: 5,200 kg
Apogee: 2000 km
First launch: 1961 |
|
RAM-A
Engines:
0. 2 × Recruit | XM-19 /
1. 1 × Castor-1 | XM-33E-3
2. 1 × Skat | XM-45
3. 1 × Skat | XM-45
4. 1 × Recruit | XM-19E
Apogee: 100 km
First launch: 1961 |
|
WASP
Engines:
0. 2 × Recruit | XM-19
1. 1 × Pollux | XM-33E2
2. 1 × Antares
Total mass: 6,800 kg
Apogee: 240 km
First launch: 1966 |
|
Journeyman (Argo-D8)
Engines:
0. 2 × Recruit | XM-19
1. 1 × Sergeant | TX-20-6
2. 1 × Lance | TX-77
3. 1 × Lance | TX-77
4. 1 × Altair | × -248
Total mass: 6,300 kg
Apogee: 3,000 km
First launch: 1960 |
|
Athena RTV
Engines:
0. 2 × Recruit | XM-19
1. 1 × Castor-1
2. 1 × Pedro | TX-261-3
3. 1 × Alcor
4. 1 × Alcyone | BE-3
Total mass: 7,300 kg
Apogee: 200 km
First launch: 1964 |
|
Shotput
Engines:
0. 2 × Recruit | XM-19
1. 1 × Pollux | XM-33E2
2. 1 × Altair | × -247
Total mass: 5,100 kg
Apogee: 400 km
First launch: 1959 |
|
Trailblazer-2
Engines:
0. 2 × Recruit | XM-19
1. 1 × Sergeant | TX-20-6
2. 1 × Lance | TX-77
3. 1 × Altair | × -248
4. 1 × Cygnus-15
5. 1 × Cygnus-5
Total mass: 6,100 kg
Apogee: 300 km
First launch: 1961 |
|
ARPAT Target
Engines:
0. 2 × Recruit | XM-19
1. 1 × Castor-1
2. 1 × Pedro | TX-261
Total mass: 4,000 kg
Apogee: 30 km
First launch: 1962 |
|
| |
|
Trailblazer-1
Engines:
1. 1 × Honest John
2. 1 × Nike
3. 1 × Lance
4. 1 × T-50
5. 1 × T-55
6. 1 × Cygnus 5
Apogee: 280 km
First launch: 1959 |
|
Exos (Argo-B7)
Engines:
1. 1 × Honest John
2. 1 × Nike |
|
Exos (Argo-C16)
Engines:
1. 1 × Honest John
2. 1 × Nike
3. 1 × Yardbird | TE-291
Apogee: 600 km |
|
Javelin (Argo-D4)
Engines:
1. 1 × Honest John
2. 1 × Nike
3. 1 × Nike
4. 1 × Altair | × -248
Apogee: 1,100 km
First launch: 1959 |
|
Jason (Argo-E5)
Engines:
1. 1 × Honest John
2. 1 × Nike
3. 1 × Nike
4. 1 × Recruit
5. 1 × T-55
Apogee: 800 km
First launch: 1958 |
|
|
|
|
Hermes-A1, A3
Engines: Wf
Total mass: 3,025 kg
Apogee: 25 km
First launch: 1950 |
|
|
|
|
Viking 1 / 2
Engines:
1. 1 × XLR-10
Total mass: 4,500 kg / 6,800 kg
Ceiling: 200 / km 250 km
First launch: 1949 / 1952 |
|
Vanguard - TV
Engines:
1. 1 × XLR-10
Launches: 2 (Failures: 0)
/1956-1957/ |
|
|
|
|
| Vanguard |
|
|
|
|
|
|
Vanguard
Engines:
1. 1 × × -405
2. 1 × AJ10-37
3. 1 × GCRC
1 × X-248
Total mass: 10,050 kg
Payload:
(LEO) 9 kg
20 kg |
(GCRC)
(X-248) |
|
|
Launches: 12 (Failures: 8)
/1957-1959/
|
|
Retired |
|
| |
|
Redstone
Engines:
1. 1 × A-6
Total mass: 27,800
kg
Apogee: 92 km
Maximum range: 325 km
Warhead: 3,580 kg / 4
MT
First launch: 1953
Operational Capability: 1958 |
|
Launches: 52 (Failures: 9)
/1966-1967/
|
|
|
|
| Jupiter C |
|
|
|
|
|
Jupiter C
Engines:
1.
2.
3. |
1 ×
11 ×
3 × |
A-7
Baby Sergeant
Baby Sergeant |
Total mass: 29,060 kg
Apogee: 1,000
km
Fairing:
|
|
Launches: 3
/1956-1957/
|
Payload: Jupiter Composite RTV
(Reentry Test Vehicle) |
|
|
Retired |
|
|
|
| Juno 1 |
|
|
|
|
|
Juno 1
Engines:
1.
2.
3.
4.
|
1 ×
11 ×
3 ×
1 × |
A-7
Baby Sergeant
Baby Sergeant
Baby Sergeant
|
 |
| JPL 2lb Motor |
Total mass: 29,060 kg
Payload (LEO): 11 kg
Fairing:
(1) |
|
Launches: 6 (Failures: 3)
/1956-1958/
|
Payload: Explorer, Beacon |
|
|
Retired |
|
|
|
|
| Redstone Sparta |
|
| Redstone Sparta |
|
|
|
|
|
Redstone Sparta |
Engines:
1. 1 × A-6
2. 1 × Antares-2
|
| JBE-3 (Alcyone) |
|
|
Launches: 10 (Failures: 1)
/1966-1967/
| |
L |
F |
|
suborbital
orbital |
9
1 |
1 |
/1966-1967/
/1967/ |
|
|
Retired |
|
|
|
| Redstone - Mercury |
|
|
|
|
Redstone - Mercury
Engines:
1. 1 × A-6
|
| 3 × TE-M-316 (retro motor) |
Total mass: 28,440 kg |
|
Launches:
suborbital: 6 (Failures: 1)
/1960-1961/
|
|
Retired |
|
|
|
| Jupter |
 |
|
|
|
|
Jupter (PGM-19)
Engines:
1. 1 × S-3D
Total mass: 49,800 kg
Apogee: 500 km
Maximum range: 2980 km
First launch: 1957
Operational Capability: 1960 |
|
Launches: 36 (Failures: 6)
/1957-1963/
|
|
Retired |
|
|
|
| Juno 2 |
|
|
|
|
|
Juno 2
Engines:
1.
2.
3.
4. |
1 ×
11 ×
3 × 1 × |
S-3D
Baby Sergeant
Baby Sergeant
Baby Sergean |
Total mass: 55,110
Apogee: 200 km
Payload (LEO): 41 kg
Fairing:
(2) |
|
Launches: 10 (Failures: 6)
/1958-1961/
|
Payload: Pioneer, Explorer, Beacon |
|
|
Retired |
|
|
|
| Thor |
|
|
|
|
Thor DM18 (SM-75)
Engines:
1. 1 × MB-3-1
Total mass: 49,800 kg
Maximum range: 2,400 km
Apogee: 480 km
First launch: 1957
Operational Capability: 1957 |
|
|
|
|
| Little Joe 1 |
|
|
|
| |
|
|
|
Little Joe 1
Engines:
1. 2 × Pollux
1. 4 × Pollux
1. 4 × Castor |
+ 4 × Recruit
+ 4 × Recruit
+ 4 × Recruit |
Total mass: 12,700 kg
Apogee: 89 km |
|
Launches: 7 (Failures: 4)
/1959-1961/
|
|
Retired |
|
|
|
| Little Joe 2 |
|
|
|
| |
|
|
Little Joe 2
Engines:
1. 1 × Algol-1D + 6 × Recruit
1. 2 × Algol-1D + 4 × Recruit
1. 4 × Algol-1D + 5 × Recruit
1. 6 × Algol-1D
Total mass: 63,300 kg
Apogee: 23 km |
|
Launches: 5 (Failures: 0)
/1963-1966/
|
Payload: QTV, Apollo BP (Boiler Plate) |
|
|
Retired |
|
|
|
 |
Engines:
1. 2 × XLR-89-1
2. 1 × Aerobee AJ10-25
Total mass: 82,500 kg
Apogee: 300
km
Payload (LEO): 50 kg
Status: Concept
/1956/
|
 |
Never flown |
|
Atlas A (XSM-65A)
Engines:
1. 2 × XLR-89-1
Total mass: 81,647 kg
Apogee: 120 km |
|
| |
|
Engines:
Status: Development
/cancelled 1959/
|
 |
| Payload: deep space and planetary missions, ņpace laboratory |
|
|
Never flown |
|
|
|
|
| Titan 1 |
|
|
|
|
|
Titan 1 (SM-68)
Engines:
1. 2 × LR-87-3
2. 1 × LR-91-3
Total mass: 105,142 kg
Maximum range: 11,300 km
Apogee: 1,000 km
First launch: 1959
Operational Capability: 1962 |
|
Launches: 64 (Failures: 8)
/1959-1965/
|
|
|
|
Never flown |
|
Payload:
Martin Project 7969, Aeronutronics Project 7969, Convair Project 7969,
McDonnel Project 7969
Status: Design
/1957/ |
|
|
Never flown |
|
Payload:
Goodyear Project 7969,
instrument package into lunar orbit and on the lunar surface |
|
|
Never flown |
|
|
|
|
