Encyclopedia Astronautica
SB-735


Nissan solid rocket engine. 327.8 kN. Isp=263s. Used on Mu-3S launch vehicle. First flight 1969.

Thrust (sl): 296.700 kN (66,701 lbf). Thrust (sl): 30,252 kgf.

Gross mass: 5,100 kg (11,200 lb).
Unfuelled mass: 1,080 kg (2,380 lb).
Height: 8.25 m (27.06 ft).
Diameter: 0.73 m (2.39 ft).
Thrust: 327.80 kN (73,692 lbf).
Specific impulse: 263 s.
Specific impulse sea level: 238 s.
Burn time: 38 s.
Number: 48 .

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Associated Countries
See also
Associated Launch Vehicles
  • Mu-3S Japanese all-solid orbital launch vehicle. Four stage vehicle consisting of 8 x SB-310 + 1 x M-13TVC + 1 x M-22TVC + 1 x M-3A More...

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-3S-0 Solid propellant rocket stage. Loaded/empty mass 5,100/1,080 kg. Thrust 327.83 kN. Vacuum specific impulse 263 seconds. More...

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