The Wayback Machine - https://web.archive.org/web/20161228080849/http://astronautix.com/r/rsa-4-1.html
RSA-4-1

Encyclopedia Astronautica
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
RSA-4-1
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.
See More

Status: Development ended 1994. Thrust: 1,520.00 kN (341,700 lbf). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 52 s.

Country: South Africa. Launch Vehicles: RSA-4. Propellants: Solid. Stages: RSA-4-1.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
� 1997-2016 Mark Wade - Contact
� / Conditions for Use