Encyclopedia Astronautica Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z SB-735 engine AKA: Mu-3S-0; SB-735. Status: Retired 1995. Number: 48 . Thrust: 327.80 kN (73,692 lbf). Gross mass: 5,100 kg (11,200 lb). Unfuelled mass: 1,080 kg (2,380 lb). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 38 s. Height: 8.25 m (27.06 ft). Diameter: 0.73 m (2.39 ft). Nissan solid rocket engine. Used on Mu-3S launch vehicle. First flight 1969. Mu-3S zero stage.
Country: Japan. Launch Vehicles: Mu-3S, Mu-3S-II. Propellants: Solid. Stages: SB-735 engine. Agency: Nissan. Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z � 1997-2016 Mark Wade - Contact � / Conditions for Use |
