The Wayback Machine - https://web.archive.org/web/20161228151326/http://astronautix.com/s/shtil-3a.html
Shtil-3A

Encyclopedia Astronautica
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
Shtil-3A
Part of R-29 Family
Shtil-3A
Shtil-3A
Credit: � Mark Wade
Russian intercontinental ballistic orbital launch vehicle. Proposed four-stage air-launched orbital launch vehicle based on R-29RM SLBM. Ignition mass 46 metric tons.
See More

AKA: Aerokosmos; RSM-54; SS-N-23. Status: Out of production. Payload: 950 kg (2,090 lb). Gross mass: 46,000 kg (101,000 lb). Apogee: 200 km (120 mi).

LEO Payload: 950 kg (2,090 lb) to a 200 km orbit. Payload: 620 kg (1,360 lb) to a 400 km orbit.

Family: aircraft-launched, ICBM, orbital launch vehicle. Country: Russia. Agency: Makeyev bureau.

Photo Gallery
ICBM-Derived LVsICBM-Derived LVs
The range of launch vehicles derived from decommissioned ballistic missiles offered for sale by Russia after the cold war.
Credit: � Mark Wade
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
� 1997-2016 Mark Wade - Contact
� / Conditions for Use