Aerodynamics of generalized bent biconics for aero-assisted, orbital-transfer vehicles
Author:
Affiliation:
1. Informatics General Corporation, Palo Alto, California
2. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25717
Reference11 articles.
1. Base heating on an aerobraking orbital transfer vehicle
2. Aerothermodynamic design feasibility of a generic planetary aerocapture/aeromaneuver vehicle
3. An experimental investigation of control surface effectiveness and real-gas simulation for biconics
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1. Longitudinal stability measurements of a winged biconic configuration in supersonic flow;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-09-20
2. Aerothermodynamic Data of Non-Winged Re-entry Vehicles (RV-NW) - Cones and Bicones -;Aerodynamic Data of Space Vehicles;2014
3. Aerothermodynamic Design Problems of Non-Winged Re-Entry Vehicles;Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles;2009
4. Bent-biconic single-stage-to-orbit vehicle conceptual study;Journal of Spacecraft and Rockets;1996-07
5. Calculation of real-gas effects on blunt-body trim angles;AIAA Journal;1992-04
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