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
JP-5/H2O2
Notional H2O2/Kerosene rocket engine. Study 1993. Engine for Black Horse winged, single stage to orbit launch vehicle using aerial refueling.

Status: Study 1993. Thrust: 63.00 kN (14,162 lbf). Specific impulse: 335 s. Burn time: 560 s.

Selected propellants for Black Horse winged, single stage to orbit launch vehicle using aerial refueling and lower performance, non-cryogenic propellants. Takes off from runway at 48,452 lbs gross weight; rendezvous with tanker to load 146,870 lbs oxidizer; then flies to orbit.

Propellant Formulation: H2O2/JP-5.



Family: Storable liquid. Country: USA. Launch Vehicles: Black Horse. Propellants: H2O2/Kerosene. Stages: Black Horse AV.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use