Encyclopedia Astronautica
M-30


Nissan solid rocket engine. 128 kN.

Gross mass: 2,800 kg (6,100 lb).
Unfuelled mass: 773 kg (1,704 lb).
Height: 4.00 m (13.10 ft).
Diameter: 0.86 m (2.82 ft).
Thrust: 128.00 kN (28,775 lbf).
Burn time: 42 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-3D-3 Solid rocket stage. 128.00 kN (28,776 lbf) thrust. Mass 2,800 kg (6,173 lb). More...

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