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 M-23-Mu AKA: M-23; Mu-3S-2. Status: Retired 1995. Number: 24 . Thrust: 524.00 kN (117,799 lbf). Gross mass: 13,100 kg (28,800 lb). Unfuelled mass: 2,800 kg (6,100 lb). Specific impulse: 285 s. Specific impulse sea level: 220 s. Burn time: 70 s. Height: 6.19 m (20.30 ft). Diameter: 1.41 m (4.62 ft). Thrust (sl): 404.500 kN (90,935 lbf). Thrust (sl): 41,247 kgf.
Country: Japan. Launch Vehicles: Mu-3S, Mu-3S-II. Propellants: Solid. Stages: M-23-Mu. 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 |
