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-310 AKA: Mu-3C-0. Status: Retired 1984. Thrust: 95.00 kN (21,356 lbf). Gross mass: 500 kg (1,100 lb). Unfuelled mass: 190 kg (410 lb). Burn time: 7.40 s. Height: 5.80 m (19.00 ft). Diameter: 0.31 m (1.01 ft). ISAS solid rocket engine. Mu-3C zero stage.
Country: Japan. Launch Vehicles: Lambda 2, Lambda 3, Lambda 3H, Lambda 4S, Mu-1, Mu-3D, Lambda 4T, Mu-4S, Lambda 4SC, Mu-3C, ETV, Mu-3H, Mu-3S. Propellants: Solid. Stages: SB-310. Agency: ISAS. 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 |
