|
17D58E
|
|
Government Designation: 17D58E. Designer: Isayev. Application: Rokot-3 Briz; Soyuz-2 Briz; Proton Briz-M vernier. Propellants: N2O4/UDMH. Thrust(vac): 13 N (3 lbf). Isp: 247 sec. Burn time: 3,200 sec. Chambers: 1. Oxidizer to Fuel Ratio: 2.00. Country: Russia. Status: In Production. High performance storable liquid engine. Manufactured by Isayev. Small attitude control thruster in Briz upper stage propulsion system S5.98M. Minimum impulse 0.068 kg-s. Specific impulse also reported as 270 sec.
Bibliography and Further Reading - Chemiy, I, Novosti kosmonavtiki, "'Rokot' - nekotrie deali", Issue 3, 1999, p. 53..
- Haeseler, Dietrich, "Personal communication", 1998 December..
|
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.
© Mark Wade, 1997 - 2007 except where otherwise noted.
|
|
|
|