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Conceptual design assessment of a suborbital tourist space access vehicle

Published online by Cambridge University Press:  03 February 2016

B. Chudoba ,
G. Coleman ,
X. Huang  and
P. A. Czysz
B. Chudoba
Affiliation:
The University of Texas at Arlington, Arlington, Texas, USA
G. Coleman
Affiliation:
The University of Texas at Arlington, Arlington, Texas, USA
X. Huang
Affiliation:
The University of Oklahoma, Norman, Oklahoma, USA
P. A. Czysz
Affiliation:
HyperTech Concepts LLC, St Louis, Missouri, USA
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Abstract

Space transportation remains in the pioneering stages. What might this century bring if we had a ‘railroad to space’ that embodied the characteristics of the transcontinental undertaking? The X-33 and Venture Star projects were one attempt to achieve the characteristics of that transcontinental railroad. There are others, here and in other countries, but perhaps we need to begin with a smaller first step, a small, commercial reusable rocket with ballistic ascent to space altitude with a hypersonic glider return? Our challenge in space today is to develop vehicles that are in continuous use, maintained and operated on a fixed schedule despite weather or environmental hazards, which move payloads not only into space but back again. The X PRIZE was a $10 million prize awarded to Scaled Composites as the first privately financed spaceship that launched the equivalent of three persons to an altitude of at least 100 kilometers on two consecutive flights within two weeks. What about an analogous vehicle that flies two or three times a week, every week for a number of years? A major difference is that this challenge is to be accomplished without government support or government developed vehicles. The aerospace vehicle design (AVD) Laboratory team at the University of Texas at Arlington is developing a generic space access vehicle (SAV) design synthesis environment with focus on the conceptual design phase. The AVD Lab has applied elements of this toolbox to the study of a tourist aerospace vehicle under a grant from Rocketplane Limited, Inc. The development of a low-cost tourist vehicle based on the adaptation of a Learjet 25/35/45 series aircraft is the focus of this paper.

Type
Research Article
Information
The Aeronautical Journal , Volume 112 , Issue 1135 , September 2008 , pp. 523 - 535
Copyright
Copyright © Royal Aeronautical Society 2008 

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References

1. Czysz, P.A., Chudoba, B., and Rahaim, C., Low earth orbit infrastructure configuration and requirements translated Into support Vehicle requirements, AIAA Paper, AIAA-2008-2543, 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, USA, 28 April – 1 May 2008.Google Scholar
2. Chudoba, B., Coleman, G., Huang, X. and Czysz, P.A., Conceptual design assessment of a suborbital tourist space access vehicle (SAV), AIAA Paper, AIAA-2006-1240, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 9-12 January 2006.Google Scholar
3. Urie, D., Rocketplane XP – An advanced space transportation concept, presentation to FAA/AST, 1 March 2004.Google Scholar
4. Huang, X. and Chudoba, B., Overview of a HTHL hands-on SAV design synthesis methodology, AIAA Paper, AIAA-2007-241, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 8-11 January 2007.Google Scholar
5. Huang, X. and Chudoba, B., Application of a HTHL SAV design methodology for a suborbital tourism vehicle, AIAA Paper, AIAA-2007-242, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 8-11 January 2007.Google Scholar
6. Huang, X., Chudoba, B. and Coleman, G., A generic hands-on conceptual design methodology applied to a tourist space access vehicle, AIAA Paper, AIAA-2006-1242, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 9-12 January 2006.Google Scholar
7. Roberts, K., Mixon, B., Chudoba, B. and Huang, X., A unique conceptual design approach: generic design space screening and convergence of hypersonic vehicles, AIAA Paper, AIAA-2006-1241, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 9-12 January 2006.Google Scholar
8. Roberts, K. and Chudoba, B., Flight vehicle design heritage: are we on the road to Alexandria?, AIAA Paper, AIAA-2007-657, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 8-11 January 2007.Google Scholar
9. Coleman, G., Chudoba, B. and Huang, X., Assessment of current space access vehicle tourism regulations and their implications on design, AIAA Paper, AIAA-2006-1528, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 9-12 January 2006.Google Scholar
10. Chudoba, B. and Huang, X., Development of a dedicated aerospace vehicle conceptual design knowledge-based system, AIAA Paper, AIAA-2006-0225, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 9-12 January 2006.Google Scholar
11. Chudoba, B., Stability and Control of Conventional and Unconventional Aircraft Configurations – A Generic Approach, 1st Ed, Books on Demand, April 2001 [ISBN 3-8311-2982-7].Google Scholar
12. Chudoba, B., Stability and control characteristics of subsonic, supersonic, and hypersonic aircraft configurations, CoA Report NFP0103, Department of Aerospace Technology, College of Aeronautics, Cranfield University, April 2001.Google Scholar
13. Chudoba, B., Aircraft configuration characterisation For ‘project flight mechanics’, Issue 1, CoA Report NFP0106, College of Aeronautics, Cranfield University, April 2001.Google Scholar
14. Chudoba, B., Investigation of inherent slender-body characteristics using the CONCORDE Simulator, CoA Report NFP0104, Department of Aerospace Technology, College of Aeronautics, Cranfield University, 27 February 1997.Google Scholar
15. Vandenkerckhove, J.A. and Czysz, P.A., Transatmospheric vehicle sizing, in scramjet propulsion, progress in astronautics and aeronautics series, V-189, AIAA, 2001.Google Scholar
16. Czysz, P.A., Hypersonic convergence, AEP-452, Parks College of Engineering and Aviation, AEP-452, Saint Louis University, September 1995.Google Scholar
17. Chudoba, B., Striz, F. and Huang, X., et al, Conceptual Design Support for Rocketplane Limited, Inc. Model XP ‘Space Sooner’ – Phase I, AVD/RLI-CD1-2004, Final Phase 1 Contract Report, AVD Laboratory, The University of Oklahoma, 16 September 2004.Google Scholar
18. Chudoba, B., Coleman, G. and Huang, X., Model XP Conceptual Design Wing Planform Selection – Phase 2, AVD/RLI-CD2-2004, Final Phase 2 Contract Report, AVD Laboratory, The University of Oklahoma, 19 October 2004.Google Scholar
19. Chudoba, B., Czysz, P.A., Ferguson, A. and Baird, B., Model XP ‘Space Sooner’ Wind Tunnel Campaign – Phase 1, AVD/RLI-WT1-2005, Contract Report, AVD Laboratory, The University of Oklahoma, Oklahoma, UK, 15 February 2005.Google Scholar
20. Huang, X., A Prototype Computerized Synthesis Methodology for Generic Space Access Vehicle (SAV) Conceptual Design, PhD Dissertation, AVD Laboratory, The University of Oklahoma, Oklahoma, UK, 2006.Google Scholar
21. Chudoba, B. and Czysz, P.A., Necessary volume and size for design convergence, AE 5367 High-speed aircraft and space access vehicle design, Fall Semester 2007, The University of Texas at Arlington, Texas, USA, November 2007.Google Scholar
22. Coleman, G., Chudoba, B. and Huang, X., Assessment of Current Space Access Vehicle Tourism Regulations and Their Implications on Design, AIAA Paper, AIAA-2006-1528, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 9-12 January 2006.Google Scholar
23. Shevell, R.S., Fundamentals of Flight, 2nd Ed, Prentice-Hall, Inc, 1989.Google Scholar
24. Chudoba, B. and Czysz, P.A., Orbital Sciences X-34 Stability and Control, Memo to Rocketplane Limited, Inc., AVD Lab, The University of Oklahoma, 17 January 2005.Google Scholar
25. Pamadi, B.N., Brauckmann, G.J., Ruth, M.J. and Fuhrmann, H.D., Aerodynamic characteristics, database development and flight simulation of the X-34 vehicle, AIAA Paper, AIAA 2000-09, 10-13 January 2000.Google Scholar
26. Dornheim, M.A., SpaceShipOne – FAA Administrators hints spaceship may be treated like experimental aircraft, Aviation Week & Space Technology, 11 October 2004.Google Scholar
27. Jenkins, D.R. and Landis, T.R., Hypersonic – The Story of the North American X-15, 1st Ed, Specialty Press, 2003.Google Scholar
28. Carlier, C. and Berger, L., Dassault – The Programs, 1st Ed, Dassault Aviation, 1996.Google Scholar
29. Orlebar, C., The Concorde Story, 5th Ed, Hamlyn Publishing Group, 1994.Google Scholar
30. Hoak, D.E. and Finck, R.D., et al, USAF Stability and Control Datcom, Flight Control Division, Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, 1978.Google Scholar
31. Anderson, J.D., Modern Compressible Flow with Historic Perspective, 1st Ed, McGraw-Hill, New York, 1982.Google Scholar
32. Rutowsky, R.S., Energy approach to the general aircraft performance Problem, J Aerospace Sciences, 21, 1954, pp 187–195.Google Scholar