![]() 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 KTDU-35 AKA: 11D62;S5.35 + S5.60. Status: Out of Production. Date: 1962-67. Thrust: 4.09 kN (919 lbf). Unfuelled mass: 305 kg (672 lb). Specific impulse: 280 s. Burn time: 500 s. Height: 1.14 m (3.73 ft). Diameter: 2.50 m (8.20 ft).
Chambers: 1 + 2. Engine: 305 kg (672 lb). Chamber Pressure: 39.20 bar. Propellant Formulation: AK27I/UDMH. Thrust to Weight Ratio: 1.36. Oxidizer to Fuel Ratio: 1.85. Coefficient of Thrust sea level: 0.
Family: Storable liquid. Country: Russia. Spacecraft: Soyuz A PAO, Soyuz 7K-OK Tether, Soyuz 7K-OK, Soyuz 7K-OK PAO, Soyuz Kontakt, Soyuz 7KT-OK, Soyuz 7K-T, Soyuz 7K-T PAO, Salyut 4, Soyuz 7K-T/A9, Soyuz 7K-MF6. Propellants: Nitric acid/UDMH. Agency: Isayev bureau. Bibliography: 314, 321, 342, 7437. 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 |