Solid propellant rocket stage. Loaded mass 400 kg. Thrust 60.00 kN.
Status: Retired 1965.
Gross mass: 400 kg (880 lb).
Height: 3.00 m (9.80 ft).
Diameter: 0.35 m (1.14 ft).
Thrust: 60.00 kN (13,488 lbf).
Burn time: 10 s.
Number: 4 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
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LS-A Japanese test vehicle. Early suborbital test version of the Lambda rocket series. More...
Associated Manufacturers and Agencies
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Mitsubishi Japanese manufacturer of rockets, spacecraft, and rocket engines. Mitsubishi Electric Corp, Japan. More...
Associated Propellants
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Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...
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