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
DOK-50
Part of DOT Family
Isayev monopropellant rocket engine. In Production. Pressure-fed monopropellant engine. Thermal decomposition of hydrazine by an iridium-based catalyst, which heated to increase stability. 40,000 ignitions

Status: In Production. Thrust: 50 N (11 lbf). Unfuelled mass: 1.10 kg (2.40 lb). Specific impulse: 229 s. Burn time: 1,500 s.

Engine: 1.10 kg (2.40 lb). Chamber Pressure: 8.00 bar. Area Ratio: 42. Thrust to Weight Ratio: 4.63.



Family: Monopropellant. Country: Russia. Agency: Isayev bureau. Bibliography: 350.

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