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 Martlet 4-1 AKA: Martlet 4A; Martlet 4i-1. Status: Development ended 1966. Thrust: 67.70 kN (15,220 lbf). Gross mass: 570 kg (1,250 lb). Unfuelled mass: 110 kg (240 lb). Specific impulse: 300 s. Specific impulse sea level: 210 s. Burn time: 20 s. Diameter: 0.30 m (0.98 ft). Thrust (sl): 47.400 kN (10,656 lbf). Thrust (sl): 4,830 kgf.
Country: Canada. Launch Vehicles: Martlet 4, Martlet 3D. Propellants: Solid. Stages: Martlet 4-1. Agency: Bull. 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 |
