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What price supersonic speed? A design anatomy of supersonic transportation Part 1

Published online by Cambridge University Press:  03 February 2016

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

The first generation of supersonic commercial transportation has seen three serious attempts to arrive at an economically and environmentally viable aircraft. The US B2707-200/300 design was cancelled early before a prototype could emerge; the Russian Tu-144 design succeeded to become the first supersonic transport but spanned only a few years of restricted airline service; the Anglo-French Concorde endured more than 27 glamorous airline service years until the last of its species was retired on 30 August 2003. This first generation was followed by a second generation of supersonic commercial transport projects in the time period between 1986 until about 1999, designs which did not proceed towards the production hardware stage. This study critically examines the anatomy of two generations of supersonic commercial transport design failures and successes in order to arrive at lessons learned free of ‘wishful thinking’. The design conditions leading to the identification of the product ‘solution space’ for an economically and environmentally acceptable supersonic commercial transport are discussed. Having assembled an understanding of the product metrics valid for supersonic commercial transports, the paper then provides an outlook for the first generation of supersonic corporate and cargo jet projects. This first generation of supersonic business jet (SSBJ) and supersonic cargo jet (SSCJ) projects spans a period of nearly two decades of development, starting from 1988 until today. The present study identifies that the product development metrics of this class of aircraft is radically different compared to the metrics valid for supersonic commercial transports. The challenges in VIP transportation and dedicated freight transportation at supersonic speeds are portrayed leading to two principal trains of thought targeting the development of the first supersonic business jet and/or supersonic cargo jet hardware: the development based on a new airframe, and alternatively the development based on an existing airframe.

Type
Research Article
Information
The Aeronautical Journal , Volume 112 , Issue 1129 , March 2008 , pp. 141 - 151
Copyright
Copyright © Royal Aeronautical Society 2008 

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References

1. Chudoba, B., Coleman, G., Huang, X., Huizenga, A., Czysz, P.A. and Butler, C.M., A feasibility study of a supersonic business jet (SSBJ) based on the learjet airframe, AIAA Paper, AIAA-2006-0028, 44th AIAA Aerospace sciences meeting and exhibit, 9-12 January 2006, Reno, Nevada, USA.Google Scholar
2. Chudoba, B. and Coleman, G. et al, What price supersonic speed? a design anatomy of supersonic transportation – Part 1, AIAA Paper, AIAA-2007-851, 45th AIAA Aerospace sciences meeting and exhibit, 8-11 January 2007, USA, Reno, Nevada.Google Scholar
3. Chudoba, B. and Coleman, G. et al, What price supersonic speed? an applied market research case study – Part 2, AIAA Paper, AIAA-2007-848, 45th AIAA Aerospace sciences meeting and exhibit, 8-11 January 2007, Reno, Nevada, USA.Google Scholar
4. Rahaim, C.P. and Czysz, P.A., Supersonic cargo jet (SSCJ), ISABE-2003-1198, XVI International symposium on air breathing engines (ISABE), 31 August – 5 September 2003, Cleveland, USA.Google Scholar
5. Snow, J., The Future SST, Chapter 12 in Faster, Further, Higher – Leading-Edge Aviation Technology Since 1945, (Ed) Jarrett, P. 1st ed, Putnam’s History of Aircraft, 2002.Google Scholar
6. Yong, J., Smith, R., Hatano, L. and Hillmansen, S., What price speed – Revisited, 22, Ingenia, Railway Research Group, Imperial College, England, UK, March 2005.Google Scholar
7. Gabrielli, G. and Von Karman, T., What price speed – specific power required for propulsion of vehicles, 72, (10), Mechanical Engineering, ASME, 1950, pp 775–781.Google Scholar
8. Von Karman, T., Aerodynamics – Selected Topics in the Light of Their Historical Development, 1957, 2nd Ed, Cornell University Press.Google Scholar
9. Kelly, E., Airbus Discusses A380 Penalties, Flight International, 22-28 November 2005, p 22.Google Scholar
10. Küchemann, D., The Aerodynamic Design of Aircraft – A Detailed Introduction to the Current Aerodynamic Knowledge and Practical Guide to the Solution of Aircraft Design Problems, 1st ed, Pergamon Press, 1978.Google Scholar
11. Davies, R.E.G., Supersonic (Airliner) Non-Sense – A Case Study in Applied Market Research, 1998, 1st ed, Paladwr Press.Google Scholar
12. Anon, High-speed civil transport study – summary, Boeing commercial airplanes, new Airplane development, NASA Contractor Report 4234, Contract NAS 1-18377, September 1989, NASA Langley, USA.Google Scholar
13. Builder, C.H., On the thermodynamic spectrum of airbreathing propulsion, AIAA-64-243, First AIAA Annual Meeting, 29 June to 2 July 1964, Washington, DC, USA.Google Scholar
14. Seebass, R. and Argrow, B., Sonic boom minimization revisited, AIAA-98-2956, Theoretical Fluid Mechanics Meeting, 15-18 June 1998, 2nd ed, Albuquerque, NM, USA.Google Scholar
15. Penn, J.P. and Lindley, C.A., The Aerospace Corporation Database, Aviation Week and Space Technology, 15 June 1998.Google Scholar
16. Draper, A.C., Buck, M.L. and Goesch, W.H., A delta shuttle orbiter, Astronautics and Aeronautics, 1971, 9, (1), pp 26–36.Google Scholar
17. Froning, H.D., Requirements for rapid transport to the further stars, J British Interplanetary Society, 1983, 36, pp 227–230.Google Scholar
18. Penn, J.P. and Lindley, C.A., Spaceplane design and technology considerations over a broad range of mission applications, The Aerospace Corporation, 1998, El Segundo, California, USA.Google Scholar
19. Turnill, R., 25 Supersonic Years – Celebrating Concorde, 1994, 1st ed, Ian Allan Publishing.Google Scholar
20. Shurcliff, W.A., S/S/T and Sonic Boom Handbook – A Documented Source Book on the Supersonic Transport Planes (S/S/T’s) Now Being Developed and the Sonic Booms They Would Produce, 1st ed, Ballantine Books, February 1970.Google Scholar
21. Orlebar, C., The Concorde Story – Includes an Account of Concorde’s Final Flight – British Airways, 6th ed, Osprey Publishing, 2006.Google Scholar
22. Page, G.S., Vehicle Synthesis Programme (VSP), Douglas Aircraft Memorandum C1-E82--ACAP-86-1381, December 1986.Google Scholar
23. Czysz, P.A. and Vandenkerckhove, J., Transatmospheric Launcher Sizing, Chapter 16 in Scramjet Propulsion, (Ed) Curran, E.T. and Murthy, S.N.B., AIAA Progress in Astronautics and Aeronautics, 189, 2000.Google Scholar
24. Czysz, P.A. and Rahaim, C.P. SuperSonic cargo jet (SSCJ), ISABE 2003-1198, International symposium for air breathing engines, Cleveland, Ohio, USA, September 2003.Google Scholar