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
NII 612 kgf
Part of RDMT engine series Family
NII Mash N2O4/UDMH rocket engine. experimental 612.25 kgf / 0.071 metric tons thrust / 0.031tf. Developed. Experimental thruster, 3 thrust levels by 4 valves: 6000 N, 0.7 N, 0.3 N. Specific impulse 326 - 286 sec.

AKA: RDMT-XX. Status: Developed. Thrust: 6.00 kN (1,349 lbf). Specific impulse: 286 s.



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. 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