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LS-A
Part of LS-C Family
LS-A rocket
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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