Minimum Heating Entry Trajectories for Reusable Launch Vehicles
Author:
Affiliation:
1. Santa Clara University, Santa Clara, California 95053
2. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3384
Reference8 articles.
1. Near-optimal re-entry trajectories for reusable launch vehicles
2. Optimal trajectories for hypersonic launch vehicles
3. Approximate altitude transitions for high-speed aircraft
4. Near-optimal propulsion-system operation for an air-breathing launch vehicle
5. Near-optimal operation of dual-fuel launch vehicles
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