RSA-4-1
Engine · South Africa
Original archive entry. The text, images and links below are kept as they were written.
South African solid rocket engine. Development ended 1994. Used on RSA-4 launch vehicle. Solid propellant rocket stage. Vacuum specific impulse / thrust estimated. Sea level 139,000 kN delivered over 73 seconds. Includes 3400 kg mass of fins, interstage and upper-stage constant-diameter fairing ('sleeve') which is jettisoned after first stage burnout.
Related
- Country
- South Africa
- Launch Vehicles
- RSA-4
- Propellants
- Solid
- Stages
- RSA-4-1