S-43TM
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): 197.000 kN (44,287 lbf). Thrust (sl): 20,069 kgf. Chamber Pressure: 55.30 bar. Area Ratio: 37.68.