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
Kosmos-1
Nitric acid/UDMH propellant rocket stage. Launch count 411 orbital and ca. 300 suborbital to end 1994. Failures based on proration of failures to orbit.

AKA: 11K65;65;8K65;R-14;Skean;SS-5. Status: Active. Thrust: 1,740.02 kN (391,173 lbf). Gross mass: 87,200 kg (192,200 lb). Unfuelled mass: 5,300 kg (11,600 lb). Specific impulse: 292 s. Specific impulse sea level: 248 s. Burn time: 130 s. Height: 22.40 m (73.40 ft). Diameter: 2.40 m (7.80 ft). Span: 4.40 m (14.40 ft).

Cost $ : 10.000 million.



Subtopics

R-16-1 Nitric acid/UDMH propellant rocket stage. Range 12,000 km. TsNIIMash has 1:10 structural simulation model. Two stage ICBM with nitric acid oxidizer. Developed 1956-1961. Entered service 1961. Chief designer Yangel. Source: Placard, TsNIIMash.

Country: Ukraine. Engines: RD-216. Launch Vehicles: R-14, Kosmos 65S3, R-14U, Kosmos 11K65, Kosmos 11K65M, K65M-R, Vertikal' K65UP, K65M-RB. Propellants: Nitric acid/UDMH.

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