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 Bell 8081 AKA: XLR81-BA. Status: Out of production. Number: 156 . Thrust: 71.20 kN (16,006 lbf). Unfuelled mass: 130 kg (280 lb). Specific impulse: 285 s. Burn time: 240 s. Diameter: 1.52 m (4.98 ft). Engine: 130 kg (280 lb). Chamber Pressure: 10.00 bar. Area Ratio: 45. Propellant Formulation: RFNA/UDMH. Thrust to Weight Ratio: 55.8230769230769. Oxidizer to Fuel Ratio: 2.55. Coefficient of Thrust vacuum: 2.99603430168432. Restarts: 2.
Family: Storable liquid. Country: USA. Launch Vehicles: Thor Agena B, Atlas Agena B, Thor Agena D, Thor SLV-2A Agena B. Propellants: Nitric acid/UDMH. Stages: Agena B. Agency: Bell. 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 |
