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 Yamal launch vehicle  Yamal Credit: USAF Phillips Laboratory AKA: Yamal. Status: Study 1997. Payload: 3,900 kg (8,500 lb). In order to achieve a payload double that of the current vehicle, it would seem a high-energy Lox/LH2 upper stage would be needed. Such an improvement was proposed as far back as July 1962 (the Molniya 8K78L) but never developed. The version with the Ariane 4 upper stage would be capable of putting 3900 kg into geosynchronous transfer orbit when launched from Kourou.
Payload: 3,900 kg (8,500 lb) to a GTO, 1 deg.
Family: orbital launch vehicle. Country: Russia. Agency: Korolev bureau. Bibliography: 587. 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 |
