During the past six months the research objectives outlined in the last semi-annual report were accomplished. Specifically, these are: three-dimensional (3-D) fuel-optimal ascent trajectory of the aerospace plane and the effects of thrust vectoring control (TVC) on the fuel consumption and trajectory shaping were investigated; the maximum abort landing area (footprint) was studied; preliminary assessment of simultaneous design of the ascent trajectory and the vehicle configuration for the aerospace plane was also conducted. The work accomplished in the reporting period is summarized.
Trajectory optimization for the national aerospace plane
1993-07-01
Report
No indication
English
Trajectory Optimization for the National Aerospace Plane
NTIS | 1993
|Trajectory Optimization for the National Aerospace Plane
NTIS | 1993
|Trajectory optimization for the National Aerospace Plane
NTRS | 1993
|Trajectory Optimization for the National Aerospace Plane
NTIS | 1993
|Trajectory optimization for the National Aerospace Plane
NTRS | 1992
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