Conceptual Design Assessment of a Suborbital Tourist Space Access Vehicle (SAV)-Reference-Cited by-同舟云学术

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Conceptual Design Assessment of a Suborbital Tourist Space Access Vehicle (SAV)

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Chudoba Bernd¹,Coleman Gary¹,Huang Xiao²,Czysz Paul³

Affiliation:

1. University of Texas at Arlington

2. University of Oklahoma

3. HyperTech Concepts LLC

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-1240

Reference19 articles.

1. 3Chudoba,B."Stability andControlCharacteristicsofSubsonic,Supersonic,andHypersonicAircraftConfigurations,"CoA Report NFP0103, DepartmentofAerospace Technology, Collegeof Aeronautics,Cranfield University, April 2001

2. 4Chudoba, B. "Aircraft Configuration Characterisation For `Project Flight Mechanics'," Issue 1, CoA Report NFP0106, College ofAeronautics, Cranfield University, April 2001

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Sizing Boeing X-20 DYNA-SOAR with USAF Space Planner’s Guide;AIAA SPACE 2014 Conference and Exposition;2014-08-01

2. Application of a HTHL SAV Design Methodology to Suborbital Tourism Vehicle;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

3. Overview of a HTHL Hands-On SAV Design Synthesis Methodology;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

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