Affiliation:
1. University of Oklahoma
2. Rocketplane Ltd.
Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. Pioneer Rocketplane Conceptual Design Study
2. X-34 Vehicle Aerodynamic Characteristics
3. Validation of computational Euler solutions for a high speed business jet
4. 4Engel, C.D. "Orbital Entry Aerodynamic Heating Evaluator",Qualis Technical Report [01050]-TR-2002-13, NAS8-01050, Sept. 2002.
5. 5RaymerD.P.,AircraftDesign:AConceptualApproach,AIAA3rdeditionEducationSeries,September1999.