| M-40 |
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Model: LS-A-1. Gross Mass: 400 kg (880 lb). Thrust (vac): 60.000 kN (13,488 lbf). Burn time: 10 sec. Propellants: Solid. Diameter: 0.35 m (1.14 ft). Length: 3.00 m (9.80 ft). Country: Japan. No Engines: 1. Motor: LS-A Booster. Status: Retired 1965. First Flight: 1963. Last Flight: 1965. No Launched: 4. Used as: STA S. Release conditions: Mitsubishi.
Model: Mu-4S-4. Gross Mass: 400 kg (880 lb). Empty Mass: 73 kg (160 lb). Thrust (vac): 26.500 kN (5,957 lbf). Burn time: 40 sec. Propellants: Solid. Diameter: 0.79 m (2.59 ft). Length: 1.80 m (5.90 ft). Country: Japan. No Engines: 1. Motor: M-40. Status: Retired 1972. First Flight: 1966. Last Flight: 1972. No Launched: 6. No Failed: 1. Used as: M-40. Release conditions: Nissan.
Used on Launch Vehicles:
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