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
S-43
IAE solid rocket engine. Used on VLS launch vehicle. First flight 1985.

Status: Active. Number: 20 . Thrust: 303.00 kN (68,117 lbf). Gross mass: 8,425 kg (18,573 lb). Unfuelled mass: 1,245 kg (2,744 lb). Specific impulse: 265 s. Specific impulse sea level: 225 s. Burn time: 59 s. Height: 9.00 m (29.50 ft). Diameter: 1.00 m (3.20 ft).

Thrust (sl): 262.000 kN (58,899 lbf). Thrust (sl): 26,740 kgf. Chamber Pressure: 56.20 bar. Area Ratio: 12.82.



Subtopics

S-43TM IAE solid rocket engine. Used on VLS launch vehicle. First flight 1985.

Country: Brazil. Launch Vehicles: Sonda 4, VLS, VLS-R1, VLS-1. Propellants: Solid. Stages: S-43. Agency: IAE.

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