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
RDMT-12
Part of RDMT engine series Family
Isayev / NII Mash N2O4/UDMH 12-13 N low-thrust attitude control thruster. Used on Almaz, Kvant, Kristall, Spektr, and Priroda spacecraft; and in Briz and Briz-M upper stages. In Production. Predecessor was RDMT-400. Thrust given as 0.0133 N / Isp = 247 and 270 sec in S5.98M Briz, Briz-M upper stage application.

AKA: 17D58E. Status: In Production. Thrust: 12 N (2 lbf). Unfuelled mass: 0.55 kg (1.21 lb). Specific impulse: 279 s. Burn time: 3,200 s.

Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 2.18. Oxidizer to Fuel Ratio: 2.0. Minimum impulse 0.068 kg-s.



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: Proton KM-4 Briz M, Rokot-3 Briz. Agency: NII Mash. Bibliography: 336.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use