Encyclopedia Astronautica
M-10


Nissan solid rocket engine. 737 kN.

Gross mass: 26,600 kg (58,600 lb).
Unfuelled mass: 5,907 kg (13,022 lb).
Height: 13.00 m (42.00 ft).
Diameter: 1.41 m (4.62 ft).
Thrust: 737.00 kN (165,684 lbf).
Burn time: 61 s.

More... - Chronology...


Associated Countries
See also
Associated Manufacturers and Agencies
  • Nissan Japanese manufacturer of rocket engines and rockets. Nissan, 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...

Associated Stages
  • Mu-4S-1 Solid rocket stage. 737.00 kN (165,684 lbf) thrust. Mass 26,600 kg (58,643 lb). More...

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