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
5.6KS5400
Part of Viper-27
Multiple-source American solid rocket engine. Nike Viper I second stage.

AKA: Nike Viper I-2. Status: Retired 1960. Thrust: 24.00 kN (5,395 lbf). Gross mass: 90 kg (198 lb). Unfuelled mass: 25 kg (55 lb). Burn time: 5.60 s. Height: 2.70 m (8.80 ft). Diameter: 0.17 m (0.54 ft).



Country: USA. Launch Vehicles: ALSOR, Nike Viper I, Viper Falcon. Propellants: Solid. Stages: 5.6KS5400.

Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use