![]() 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 Phoenix L
Status: Study 1982-1988. Gross mass: 31,000 kg (68,000 lb). The original concepts for these vehicles were similar to the DC-Y concept of the 1990's. Nose entry was investigated, but rejected due to thermal and stability concerns.
Family: orbital launch vehicle, SSTO. Country: USA. Agency: Pacific American Launch Systems. 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 |