The work conducted by the ELORET Institute under this Cooperative Agreement includes the modeling of hypersonic propulsion systems and the evaluation of hypersonic vehicles in general and most recently hypersonic waverider vehicles. This work in hypersonics was applied to the design of a two-stage to orbit launch vehicle which was included in the NASA Access to Space Project. Additional research regarded the Oblique All-Wing (OAW) Project at NASA ARC and included detailed configuration studies of OAW transport aircraft. Finally, work on the modeling of subsonic and supersonic turbofan engines was conducted under this research program.
Advanced vehicle concepts systems and design analysis studies
1994-04-20
Report
Keine Angabe
Englisch
Advanced vehicle system concepts
Tema Archiv | 1983
|Advanced launch vehicle concepts
Engineering Index Backfile | 1963
|Advanced launch vehicle concepts
Engineering Index Backfile | 1963
|Advanced Design Concepts for Onboard LNG Vehicle Tanks
British Library Conference Proceedings | 1995
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