Parameter optimization methods were applied to maximize lateral range with and without down-range constraints to produce performance footprints. Three lifting entry vehicles with maximum lift-to-drag ratios of 1.89, 2.2, and 2.6, respectively, were used. A simplified bank control procedure was developed which closely appproximated the optimal footprint results in the case where no heating constraints were imposed.
Performance Methods for Lifting Entry Vehicle Range Analysis
1982
144 pages
Report
No indication
English
Missile Trajectories & Reentry Dynamics , Lifting reentry vehicles , Maneuverable reentry vehicles , Guided missile trajectories , Flight paths , Optimization , Angle of attack , Aerodynamic characteristics , Aerodynamic heating , Trajectories , Control systems , Lifting entry footprints , Temperature constraints , Range optimization , Simplified control , Mapping and display , Footprints , Cross range solutions , Down range solutions , Entry vehicle performance
Lifting entry rescue vehicle configuration
AIAA | 1988
|Lifting entry rescue vehicle configuration
AIAA | 1990
|Maximum range three-dimensional lifting planetary entry
TIBKAT | 1972
|Some considerations of performance of maneuverable, lifting-body, entry vehicle
Engineering Index Backfile | 1963
|The first manned lifting entry vehicle configuration
AIAA | 1966
|