S-40TM
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): 155.000 kN (34,845 lbf). Thrust (sl): 15,764 kgf. Chamber Pressure: 57.20 bar. Area Ratio: 25.97.