Encyclopedia Astronautica
LS-C-2


Solid propellant rocket stage. Loaded mass 300 kg.

Status: Retired 1974.
Gross mass: 300 kg (660 lb).
Height: 4.00 m (13.10 ft).
Diameter: 0.60 m (1.96 ft).
Number: 8 .

More... - Chronology...


Associated Countries
Associated Engines
Associated Launch Vehicles
  • LS-C Japanese test vehicle. Two stage vehicle consisting of 1 x LS-C Booster + 1 x LS-C More...

Associated Manufacturers and Agencies
  • Mitsubishi Japanese manufacturer of rockets, spacecraft, and rocket engines. Mitsubishi Electric Corp, Japan. More...

Associated Propellants
  • 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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