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LS-A
Part of LS-C
LS-A rocket Credit: NASDA |
Japanese test vehicle. Early suborbital test version of the Lambda rocket series.
Status: Retired 1965. First Launch: 1963-08-10. Last Launch: 1965-11-22. Number: 4 . Thrust: 60.00 kN (13,488 lbf). Gross mass: 800 kg (1,760 lb). Height: 7.50 m (24.60 ft). Diameter: 0.35 m (1.14 ft). Apogee: 150 km (90 mi).
2 stage vehicle consisting of 1 x LS-A Booster + 1 x LS-A
Subtopics
| K10S ISAS solid rocket engine. Kappa 10S third stage. |
| LS-A engine Mitsubishi solid rocket engine. LS-A second stage. |
Family:
test vehicle.
Country:
Japan.
Launch Sites:
Niijima.
Stages:
LS-A engine,
LS-A Booster.
Agency:
Mitsubishi.
1963 August 10 - .
03:17 GMT - .
Launch Site:
Niijima.
LV Family:
LS-C.
Launch Vehicle:
LS-A.
- Test mission - .
Nation: Japan.
Agency: STA.
Apogee: 50 km (31 mi).
1964 July 22 - .
02:50 GMT - .
Launch Site:
Niijima.
LV Family:
LS-C.
Launch Vehicle:
LS-A.
- Test mission - .
Nation: Japan.
Agency: STA.
Apogee: 150 km (90 mi).
1964 July 22 - .
08:55 GMT - .
Launch Site:
Niijima.
LV Family:
LS-C.
Launch Vehicle:
LS-A.
- Test mission - .
Nation: Japan.
Agency: STA.
Apogee: 150 km (90 mi).
1965 November 22 - .
06:35 GMT - .
Launch Site:
Niijima.
LV Family:
LS-C.
Launch Vehicle:
LS-A.
- Test mission - .
Nation: Japan.
Agency: STA.
Apogee: 150 km (90 mi).
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