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S-160
Japanese ISAS sounding rocket. Single stage vehicle.
Status: Retired 1972. First Launch: 1964-07-28. Last Launch: 1972-04-16. Number: 23 . Gross mass: 100 kg (220 lb). Height: 4.00 m (13.10 ft). Diameter: 0.16 m (0.52 ft). Apogee: 80 km (49 mi).
Subtopics
| S-A engine Mitsubishi solid rocket engine. S-A first stage. |
| HM-16 engine Mitsubishi solid rocket engine. HM-16 first stage. |
| K160 ISAS solid rocket engine. Kappa 8L second stage. |
| NAL-16 engine Mitsubishi solid rocket engine. NAL-16 first stage. |
| S-C engine Mitsubishi solid rocket engine. S-C first stage. |
| S-B engine Mitsubishi solid rocket engine. S-B first stage. |
Country:
Japan.
Propellants:
Solid.
Launch Sites:
Kagoshima,
Syowa Base.
Agency:
ISAS,
Nissan.
1964 July 28 - .
02:08 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Propellant test - .
Nation: Japan.
Agency: ISAS.
Apogee: 44 km (27 mi).
1965 July 21 - .
02:23 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Spin test - .
Nation: Japan.
Agency: ISAS.
Apogee: 9.00 km (5.50 mi).
1965 July 21 - .
05:20 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Test mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 14 km (8 mi).
1965 August 25 - .
00:15 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Booster test - .
Nation: Japan.
Agency: ISAS.
Apogee: 2.00 km (1.20 mi).
1965 August 25 - .
02:09 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Booster test - .
Nation: Japan.
Agency: ISAS.
Apogee: 9.00 km (5.50 mi).
1965 November 1 - .
02:15 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Propellant test - .
Nation: Japan.
Agency: ISAS.
Apogee: 93 km (57 mi).
1965 November 4 - .
07:25 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Despin test - .
Nation: Japan.
Agency: ISAS.
Apogee: 35 km (21 mi).
1966 April 25 - .
04:15 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Instrument test - .
Nation: Japan.
Agency: ISAS.
Apogee: 68 km (42 mi).
1967 January 24 - .
08:00 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Meteorological Test Aeronomy mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 86 km (53 mi).
1967 January 27 - .
02:15 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Instrument test - .
Nation: Japan.
Agency: ISAS.
Apogee: 86 km (53 mi).
1968 September 10 - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Test mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 80 km (49 mi).
1968 September 10 - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Test mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 80 km (49 mi).
1968 September 12 - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Test mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 80 km (49 mi).
1968 September 14 - .
01:00 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Aeronomy mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 82 km (50 mi).
1968 September 14 - .
04:00 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Aeronomy mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 82 km (50 mi).
1969 August 25 - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Instrumentation Test Aeronomy mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 78 km (48 mi).
1970 January 23 - .
05:00 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Meteorological Test Aeronomy mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 75 km (46 mi).
1970 February 10 - .
12:30 GMT - .
Launch Site:
Syowa Base.
Launch Vehicle:
S-160.
- Auroral mission - .
Nation: Japan.
Agency: NIPR.
Apogee: 87 km (54 mi).
1970 February 17 - .
12:10 GMT - .
Launch Site:
Syowa Base.
Launch Vehicle:
S-160.
- Auroral mission - .
Nation: Japan.
Agency: NIPR.
Apogee: 88 km (54 mi).
1971 April 30 - .
10:00 GMT - .
Launch Site:
Syowa Base.
Launch Vehicle:
S-160.
- Auroral mission - .
Nation: Japan.
Agency: NIPR.
Apogee: 83 km (51 mi).
1971 September 29 - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Parachute test - .
Nation: Japan.
Agency: ISAS.
Apogee: 80 km (49 mi).
1972 February 21 - .
02:00 GMT - .
Launch Site:
Kagoshima.
Launch Vehicle:
S-160.
- Fields mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 81 km (50 mi).
1972 April 16 - .
23:42 GMT - .
Launch Site:
Syowa Base.
Launch Vehicle:
S-160.
- Ionosphere mission - .
Nation: Japan.
Agency: NIPR.
Apogee: 86 km (53 mi).
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