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

---

Press Fed

---

Status: Design concept 1960's. Thrust: 17.80 kN (4,002 lbf). Unfuelled mass: 41 kg (90 lb). Specific impulse: 300 s. Diameter: 0.67 m (2.19 ft).

Engine: 41 kg (90 lb). Area Ratio: 98. Thrust to Weight Ratio: 44.3436633912824. Coefficient of Thrust vacuum: 0. Coefficient of Thrust sea level: 0.