SLV-1
Engine · India
Original archive entry. The text, images and links below are kept as they were written.
ISRO solid rocket engine. Used on ASLV, PSLV, SLV. First flight 1979.
Thrust (sl): 454.900 kN (102,266 lbf). Thrust (sl): 46,389 kgf. Chamber Pressure: 43.00 bar. Area Ratio: 6.7.
Subtopics
- Agni St2 DRDO solid rocket engine. Agni 2 second stage.
- Agni engine DRDO solid rocket engine. Agni 2 first stage.
- Prithvi engine HAL solid rocket engine. Agni TD second stage.