Von Braun-3 (original) (raw)

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

Von Braun-3

Part of Von Braun-2

Notional Nitric acid/UDMH rocket engine. Study 1952. Used on Von Braun launch vehicle.

Status: Study 1952. Thrust: 392.30 kN (88,193 lbf). Specific impulse: 286 s. Specific impulse sea level: 230 s. Burn time: 84 s.

Thrust (sl): 315.500 kN (70,927 lbf). Thrust (sl): 32,168 kgf. Propellant Formulation: WFNA/UDMH.

Subtopics

Von Braun 1948-3 Nitric acid/Hydrazine propellant rocket stage. .

Von Braun 1952-3 Nitric acid/Hydrazine propellant rocket stage. .

Family: Storable liquid. Country: Germany. Launch Vehicles: Von Braun 1952. Propellants: Nitric acid/UDMH. Stages: Von Braun 1952-3.

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