S-43
Engine · Brazil
Original archive entry. The text, images and links below are kept as they were written.
IAE solid rocket engine. Used on VLS launch vehicle. First flight 1985.
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.