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
TE-388
Thiokol solid rocket engine. Nike Iroquois second stage.

AKA: Nike Iroquois-2. Status: Retired 1979. Thrust: 24.40 kN (5,485 lbf). Gross mass: 100 kg (220 lb). Unfuelled mass: 43 kg (94 lb). Burn time: 7.70 s. Height: 2.70 m (8.80 ft). Diameter: 0.20 m (0.65 ft).



Country: USA. Launch Vehicles: Nike Iroquois. Propellants: Solid. Stages: TE-388. Agency: Thiokol.

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