Abstract
As presented in Chap. 2, airbreathing propulsion advocates have been fighting a losing battle to change the space launcher paradigm from expendable rockets, that are launched for the first, last, and only time, to sustained-use launchers that are more like military airlift transports with long and frequent usage.
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsBibliography
Ahern, J.E. (1983) Briefing for Robert Williams on Second Law Thermodynamics, DARPA Copper Canyon manager, Washington, DC, 1983.
Ahern, J.E. (1992) “Thermal Management of Air-Breathing Propulsion Systems”, AIAA Paper 92-0514, 30th Aerospace Sciences Meeting, Reno, Nevada, January 1992.
Anfimov, N.A. (1997) “In Searching for an Optimal Concept of Future Russian Reusable Space Transportation System”, in: Proceedings of the International Workshop on Spaceplane/RLV Technology Demonstrators, Tokyo, Japan, 10–12 March 1997, pp. 67–96.
Anon. (1963) “Marquardt Needs Advanced Propulsion Engineers”, Full-Page Advertisement, Aviation Week & Space Technology, 20 May 1963.
Anon. (1967) “A Study of Advanced Airbreathing Launch Vehicles with Cruise Capability”, Lockheed Report IR 21042, The Lockheed Aircraft Corporation, 1967.
Anon. (1985) “Single-Stage-to-Orbit Concept Comparison’, Aerospace Corporation, 86-2602-301-ADA, October 1985.
Anon. (2014) “Stratolaunch Eagles’, Stratolaunch Systems, Orbital ATK, 2014.
Anon. (2015a) “Space Launch System at a Glance”, NP-2015-09-83-MSFC, Marshall Space Flight Center, NASA, September 2015.
Anon. (2015b) “Declassified Manned Orbiting Laboratory (MOL) Records”, National Reconnaissance Office, October 2015.
Anon. (2016) Virgin Galactic – Human Spaceflight Vehicles Fact Sheet”, Virgin Galactic, February 2016.
Aoki, T. and Ogawara, A. (1988) “Study of LACE Cycle for SSTO Space Plane”, Paper IAF-88-252, presented at the 39th International Astronautical Federation Congress, Bangalore, India, 08–15 October 1988.
Balepin, V.V. (1996) “Air Collection Systems”, Developments in High-Speed-Vehicle Propulsion Systems, edited by S.N.B. Murthy and E.T. Curran, Progress in Astronautics and Aeronautics Series, Vol. 165, AIAA, Reston VA, 1996, pp. 385–419.
Balepin, V.V. and Tjurikov E.V. (1992) “Integrated Air Separation and Propulsion System for Aerospace Plane with Atmospheric Oxygen Collection”, SAE Technical Paper SAE-92-0974, Society of Automotive Engineers, Aerospace Atlantic Conference, Dayton, OH, 07–10 April 1992.
Balepin, V.V. and Hendrick, P. (1998) “Application of the KLIN Cycle to Vertical Take-Off Lifting Body Launcher”, AIAA Paper 98-1503, 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk, VA, 27–30 April 1998.
Balepin, V.V., Dulepov, N., Folomeev, E., Harchevnikova, G., et al. (1993) “Flight Liquid Oxygen Plants for Aerospace Plane: Thermodynamic and Integration Aspects”, SAE Technical Paper 931452, Society of Automotive Engineers, April 1993.
Balepin, V.V., Czysz, P.A., Maita, M. and Vandenkerckhove, J. (1995) “Assessment of SSTO Performance with In-Flight LOX Collection”, AIAA Paper AIAA-95-6047, presented at the AIAA 6th International Aerospace Planes Conference, Chattanooga, TN, 1995.
Balepin, V.V., Maita, M., Tanatsugu, N., and Murthy, S.N.B. (1996) “Deep-Cooled Turbojet Augmentation with Oxygen (Cryojet) for a SSTO Launch Vehicle”, AIAA Paper 96-3036, presented at the 32nd Joint AIAA, ASME, SAE and ASEE Propulsion Conference and Exhibit, Lake Buena Vista, FL, 1–3 July 1996.
Baranovsky, S.I., Davidenko, D.M. and Levin, V.M. (1992a) “Combustion Chamber of Ramjet for Aerospace Plane”, Vol. 3, presented at the 9th World Hydrogen Conference, Paris, June 1992, pp. 1583–1591.
Baranovsky, S.I., Davidenko, D.M. and Konovalov, I.V. and Levin, V.M. (1992b) “Experimental Study of the Hydrogen Supersonic Combustor”, Vol. 3, presented at the 9th World Hydrogen Conference, Paris, June 1992, pp. 699–1708.
Barrère, M. and Vandenkerckhove, J. (1993) ‘‘Energy Management’’, Paper ISABE 93-7016, presented at the XI International Symposium on Air Breathing Engines, Tokyo, Japan, September 1993.
Bartolotta, P.A., Buchen, E., Engelund, W.C., Huebner, L.D., Moses, P.L., Schaffer, M., Voland, R.T., Voracek, D.F. and Wilhite, A.W. (2011) “Horizontal Launch: A Versatile Concept for Assured Space Access,” NASA SP 2011-215994, Report of the NASA-DARPA Horizontal Launch Study, December 2011.
Batenin, V.M., Bityurin, V.A., Ivanov, G.S., Inozemzev, N.N. and Gorozhankin, P.A. (1997) “Electromagnetic Complex Concept for the Horizontal Start and Landing of a Reusable Air-Space Aircraft”, paper presented at the 48th International Astronautical Congress, Turin, Italy, 06–10 October 1997.
Billig, F.S. (1989) “Hypersonic Vehicles II”, Proceedings of the Short Course of Engine Airframe Integration, School of Mechanical Engineering, Purdue University, July 1989.
Billig, F. S. (1993) “The Integration of the Rocket with a Ram-Scramjet as a Viable Transatmospheric Accelerator”, AIAA Paper 93-7017, Vol. 1, Proceedings of the 11th ISABE, International Symposium on Air Breathing Engines, Tokyo, Japan, 20–24 September 1993, pp. 173–187.
Bizony, P. (2014) “The Making of Stanley Kubrick’s 2001: A Space Odyssey”, 1st Edition, Taschen, August 2014.
Bond, W.H. and Y, A.C. (1993) “Prospects for Utilization of Air Liquefaction and Enrichment System (ALES) Propulsion in Fully Reusable Launch Vehicles”, AIAA Paper AIAA-93-2025, presented at the 29th AIAA/SAE/ASME/ASEE Joint Propulsion Conference, Monterey, 28–30 June 1993.
Bottini, H., Bruno, C. and Czysz, P.A. (2003) “Is The MHD Scramjet Really An Advantage?” AIAA 2003-5046, presented at the 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, 20–23 July 2003.
Bottini, H., Bruno, C. and Czysz, P.A. (2004) “Analysis of Kerosene-Fueled MHD SCRJ Cruiser Performance”, paper AIAA 2004-4127, presented at the 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Fort Lauderdale FL, 12–14 July 2004.
Bruno,C. Czysz, P.A. and Murthy, S.N.B. (1997) “Electro-Magnetic Interactions in Hypersonic Propulsion Systems”, paper AIAA 97-3389, presented at the 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle WA, 6–9 July 1997.
Bruno, C. and Czysz, P.A. (1998) “An Electro-Magnetic-Chemical Hypersonic Propulsion System,” AIAA Paper 98-1582, presented at the AIAA 8th International Spaceplanes and Hypersonic Systems and Technologies Conference, Norfolk, Virginia, 27–30 April 1998.
Bruno, C., Golovitchev, V.I. and Tretyakov, P.K. (1998) “New Trends in Improving Hypersonic Vehicles Aerodynamics and Propulsion Flow Control by External Energy Supply”, Paper 98-0-1-08V, 21st International Symposium on Space and Technology (ISTS), Omiya, Japan, May 1998.
Buhlman, M. and Siebenhaar, A. (1995a) “The Strutjet: The Overlooked Option for Space Launch”, Paper AIAA-95-3124, presented at the 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Diego, CA, 10–12 July 1995.
Buhlman, M. and Siebenhaar, A. (1995b) “The Strutjet Engine: Exploding the Myths Surrounding High Speed Airbreathing Propulsion”, Paper AIAA-95-2475, presented at the 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Diego, CA, 10–12 July 1995.
Builder, C.H. (1964) “On the Thermodynamic Spectrum of Airbreathing Propulsion”, AIAA-64-243, 1st AIAA Annual Meeting, Washington, DC, June–July 1964.
Bunin, B.L. (1991) “Update on Douglas’ High-Speed Civil Transport Studies”, N94-33450, NASA-CP-10087, 1st High-Speed Research Workshop, Williamsburg, Virginia, 14–16 May 1991.
Burnett, D.R. and Czysz, P.A. (1963) “Supersonic Hydrogen Combustion Studies”, AEDC ASD-TDR-63-196, Project Nr. 3012, Task Nr. 301201, Aerodynamic Division, Directorate of Engineering Test, Air Force Systems Command, Wright-Patterson AFB, Ohio, April 1963.
Butrica, A.J. (2003) Single Stage to Orbit – Politics, Space Technology, and the Quest for Reusable Rocketry, The John Hopkins University Press, October 2003.
Campbell, J.W. and Taylor, C.R. (1998) “Ground-Based Laser Propulsion for Orbital Debris Removal”, in: Space Technology and Applications International Forum (STAIF)-1998, ed. by M.S. El-Genk, American Institute of Physics CP420.
Carlson, C.P.P., Kessler, R. and Schmitt, E.W. (1996) “Magnetohydrodynamic Generator Design for a Combined-Cycle Demonstration Powerplant”, Journal of Propulsion and Power, Vol.12. No. 2, March–April 1996.
Chertok, B. (2011) “Rockets and People: The Moon Race (Volume IV)”, 1st Edition, NASA SP-2011-4110, NASA History Series, NASA History Program Office, 2011.
Cocks, P.A.T., Holley, A.T., Greene, C.B. and Haas, M. (2015) “Development of a High Fidelity Simulation Capability”, AIAA paper 2015-1823, presented at the 53rd AIAA Aerospace Sciences Meeting, Kissimmee, FL, Jan. 5–9, 2015.
Cocks, P.A.T., Holley, A.T. and Rankin, B. (2016) “High Fidelity Simulations of a Non-Premixed Rotating Detonation Engine”, AIAA paper 2016-0125, presented at the 54th AIAA Aerospace Sciences Meeting, San Diego CA, Jan. 4–8, 2016.
Conway, E.M. (2008) “High-Speed Dreams: NASA and the Technopolitics of Supersonic Transportation, 1945–1999”, 1st Edition, New Series in NASA History, John Hopkins University Press, October 2008.
Curran, E.T. (1993) “The Potential and Practicality of High Speed Combined Cycle Engines”, in: Hypersonic Combined Cycle Propulsion, AGARD Conference Proceeding No. 479, AGARD, Neuilly-Sur-Seine, France, 1993, pp. Kl-9.
Czysz, P.A. (1987) “Hypersonic Convergence – Technology Interdependance Inhibits Technology Independence,” © McDonnell Douglas, April 1987, Purdue University Engine-Airframe Integration Short Course, July 1987.
Czysz, P.A. (1988) “Air Breather vs. Rocket: Is the Rocket the Only Reliable, Demonstrable Space Propulsion System?”, presented at the SAE Aerospace Atlantic Conference & Exposition, Dayton, OH, April 1993.
Czysz, P.A. (1988a) “Thermodynamic Spectrum of Airbreathing Propulsion”, SAE Technical Paper 881203, presented at the Future Transportation Technology Conference and Exposition, San Francisco, CA, 08–11 August 1988.
Czysz, P.A. (1992) “Space Transportation Systems Requirements Derived from the Propulsion Performance”, Paper IAF-92-0858, presented at the 43rd IAF (International Astronautical Federation) Congress, Washington, DC, September 1992.
Czysz, P.A. (1993a) “Rocket Based Combined Cycle (RBCC) Propulsion Systems Offer Additional Options”, in: 11th ISABE Proceedings, Vol 1, Tokyo, Japan, 20–24 September 1993, pp. 119–137.
Czysz, P.A. (1993b) “Hydrogen Combustion Studies – Revisited”, presented at the 1993 JANNAF Propulsion Meeting Conference, Monterey, CA, 15–19 November 1993.
Czysz, P.A. (1995) “Interaction of Propulsion Performance with the Available Design Space”, in: Proceedings of the XII International Symposium on Airbreathing Engines (ISABE), Melbourne, Australia, September 1995.
Czysz, P.A. (1999) “Combined-cycle Propulsion - is it the Key to Achieving Low Payload to Orbit Costs?”, ISABE Paper 99-7183, presented at the XIV International Symposium on Air Breathing Engines (ISABE), Florence, Italy, 11 September 1999.
Czysz, P.A., and Bruno, C. (2001) “MagnetoHydroDynamic Coupled Ramjet Propulsion System: A Perspective”, Paper ISABE 2001-1230, presented at the XV ISABE Symposium, Bangalore, India, September 2–7, 2001.
Czysz, P.A. and Murthy, S.N.B. (1991) “Energy Analysis of High-Speed Flight Systems”, in: High-Speed Flight Propulsion Systems, edited by S.N.B. Murthy and E.T. Curran, Progress in Astronautics and Aeronautics Series, Vol. 137, AIAA, Reston VA, pp. 183–186.
Czysz, P.A. and Richards, M.J. (1998) “Benefits from Incorporation of Combined Cycle Propulsion”, AIAA Paper 98-S.5.10, presented at the 48th International Astronautical Congress, Melbourne, Australia, October 1998.
Czysz, P.A. and Vandenkerckhove, J. (2000) “Transatmospheric Launcher Sizing” in Curran, E.T. and Murthy, S.N.B. Scramjet Propulsion, Progress in Astronautics and Aeronautics Series, Vol. 189, Reston VA., Chapter 16, 2000.
Daniau, E. (2002) “Pulse Detonation Engine: Concept, Performance and Applications”, ISU/AAAF Short Course, Versailles, France, May 2002.
Davies, R.E.G. (1998) “Supersonic (Airliner) Non-Sense: A Case Study in Applied Market Research”, Paladwr Press/Airlife Publishing Ltd, 1998.
Davies, P., Hempsell, M. and Varvill, R (2015) “Progress on Skylon and SABRE”, Paper IAF-15-D2.1.8, presented at the 66th International Astronautical Federation (IAF) Congress, Jerusalem, Israel, 12–16 October 2015.
Doublier, M., Pouliquen, M. and Scherrer, D. (1988) “Combined Engines for Advanced European Launchers”, Paper IAF-88-251, presented at the 39th International Astronautical Federation (IAF) Congress, Bangalore, India, 08–15 October 1988.
Draper, A.C. and Sieron, T.R. (1991) “Evolution and Development of Hypersonic Configurations 1958–1990”, WL-TR-91-3067, Flight Dynamics Directorate, Wright-Patterson Air Force Base, Ohio, September 1991.
DuPont, A.A. (1999) “Further Studies of Optimized Inlets for Hypersonic Turbine Engines”, ISABE 99-7039, presented at the XIV International Symposium of Air Breathing Engines (ISABE), Florence, Italy, September 1999.
Eckel, H.A. and Schall, W. (2008) “Laser Propulsion Systems”, in Advanced Propulsion Systems and Technologies: Today to 2000, edited by C. Bruno and A.G. Accettura, AIAA Progress in Astronautics and Aeronautics Series, Vol. 223, AIAA, Reston, VA., Chapter 14, March 2008.
Escher, W.J.D. (1966) “A Study of Composite Propulsion Systems for Advanced Launch Vehicle Applications – Volume 1: Summary Report”, Report 25,194, Ref.: 5402/855/5580, NASA Contract NAS7-377, Marquardt Corporation, Rockedyne Lockheed California Company, Van Nuys, CA, September 1966.
Escher, W.J.D., Flornes, B.J. et al., (1967) “A Study of Composite Propulsion Systems for Advanced Launch Vehicle Applications”, Marquardt Corporation Final Report, NASA Contract NAS7-377, Van Nuys CA, April 1967.
Escher, W.J.D. (1994) “Motive Power for Next Generation Space Transports: Combined Airbreathing + Rocket Propulsion”, private communication with P.A. Czysz, 1994.
Escher, W.J.D. (1995) “Rocket-Based Combined Cycle (RBCC) Powered Spaceliner Class Vehicles Can Advantageously Employ Vertical Takeoff and Landing (VTOL)”, AIAA Paper 95-6145, presented at the 1995 AIAA Aerospace Sciences Meeting, January 1995.
Escher, W.J.D. (1996) “A Winning Combination for Tomorrow’s Spaceliners”, Aerospace America, Vol. 34, No. 2, February 1996, pp. 38–43.
Escher, W.J.D. (1998) “A History of RBCC Propulsion in the U.S. - A Personal Recounting”, White Paper, Kaiser Marquardt, Van Nuys, CA, 1998.
Escher, W.J.D. (2001) “The Seven Operating Modes of the Supercharged Ejector Scramjet (SESJ) Combined-Cycle Engine”, Paper AIAA-2001-34041, presented at the 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Salt Lake City, Utah, 08–11 July 2001.
Escher, W.J.D. and Czysz, P.A. (1993) “Rocket-Based Combined-Cycle Powered Spaceliner Concept”, Paper IAF-93-S.4.478, presented at the 45th International Astronautical Federation Congress, October 1993.
Escher, W.J.D., Roddy, J.E. and Hyde, E.H. (2000) “Marquardt’s Mach 4.5 Supercharged Ejector Ramjet (SERJ) high-Performance Aircraft Engine Project: Unfulfilled Aspirations Ca. 1970”, Paper AIAA-2000-3109, presented at the 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, 16-19 July 2000.
Esteve, M.D. et al. (1977) “ODYSSEUS, Technology Integration for a Single Stage to Orbit Space Transport Using MHD Driven Propulsion”, Senior Design Study, Parks College of Aerospace and Aviation, Saint Louis University, St. Louis, MO, 1977.
Fermi, E. (1956) Thermodynamics, 1st Edition, Chapter 5, Dover Publications, New York, June 1956.
Flack, R.D. (2005) Fundamentals of Jet Propulsion with Applications, 1st Edition, Cambridge University Press, January 2005.
Frayling, C. (2015) “The 2001 File: Harry Lange and the Design of the Landmark Science Fiction Film”, 1st Edition, Reel Art Press, December 2015.
Gallagher, B. and Webster-Smith, R. (2015) “BAE Systems and Reaction Engines to Develop a Ground Breaking New Aerospace Engine”, Press Release, Reaction Engines and BAE Systems, 02 November 2015.
Glassman, I. and Sawyer, R.F. (1970) The Performance of Chemical Propellants, NATO AGARDograph 129, Technivision Services, Slogh (UK). Chapter II.C, January 1970.
Golovitchev, V.I. (1990), personal communication.
Goodall, J. and Miller, J. (2003) Lockheed’s SR-71 ‘Blackbird’ Family, 1st Edition, AeroFax, Midland Publishing, March 2003.
Gopalaswami, R., Gollakota, S., Venugolapan, P., Nagarathinam, M. and Sivathanu, P.A. (1988) “Concept Definition and Design of a Single-Stage-To-Orbit Launch Vehicle HYPERPLANE”, Paper IAF-88-194, presented at the 39th International Astronautical Federation (IAF) Congress, Bangalore, India, 08–15 October 1988.
Gorelov, V.A., Gladyshev, M.K. et al. (1995) “Ionization Near Hypersonic Vehicles: The Experience of Numerical, Laboratory and Flight Investigations”, paper AIAA 95-1940, presented at the 26th AIAA Plasmadynamics and Lasers Conference, San Diego, CA, 19–22 June, 1995.
Gorelov, V.A., Gladyshev, M.K., Kireev, A.Y., Korolev, A.S., Yegorov, I.V. and Byzov, V.N. (1996) “Computational and Experimental Investigations of Ionization near Hypersonic Vehicles”, Journal of Spacecraft and Rockets, Vol. 33, No. 6, November–December 1996.
Gounko, Y.P., Kharitonov, A.M., Latypov, A.F., Mazhul, I.I. and Yaroslavtsev, M.I. (2000) “Technique for Determination of Heat Fluxes and Force Characteristics of Ramjet/Scramjet Models in a Hot-Shot Wind-Tunnel”, Institute for Theoretical and Applied Mechanics SB RAS, Novosibirsk, 2000.
Graf, D.A. and Welge, H.R. (1991) “1989 High-Speed Civil Transport Studies - Summary”, NASA CR-187545, Contract NAS1-18378, HSCT Concept Development Group, Advanced Commercial Programs, McDonnell Douglas Corporation, September 1991.
Gurijanov, E.P. and Harsha, P.T. (1996) “AJAX - New Directions in Hypersonic Technology”, AIAA Paper 96-4609, presented at the 7th Aerospace Planes and Hypersonic Technologies Conference, Norfolk VA, April 1996.
Hannigan, R.J. (1994) Spaceflight in the Era of Aero-Space Planes, 1st Edition, Krieger Publishing Company, 1994.
Harford, J. (1997) Korolev: How One Man Masterminded the Soviet Drive to Beat America to the Moon, 1st Edition, John Wiley & Sons, April 1997.
Harney, D.J. (1967) “Similarity of Nonequilibrium Air Expansion in Hypersonic Nozzles”, USAF FDL-TM-67-1 (AD664084), Air Force Flight Dynamics Laboratory, Wright-Patterson AFB, Ohio, May 1967.
Harper, R.E. and Zimmerman, J.H. (1942) “An Investigation of Rocket Engine Thrust Augmentation with a Nozzle-Ejector System”, Arnold Engineering Development Center Report TRD-62-42, March 1942.
Heiser, W.H. and Pratt, D.T. (2002) “Thermodynamic Cycle Analysis of Pulse Detonation Engines”, AIAA Journal of Propulsion and Power, Vol. 18, No. 1, pp. 68–76.
Hellmold, W. (1999) Die V1 – Eine Dokumentation, 1st Edition, Bechtermünz Verlag, 1999.
Hendrick, I.P. (1996) “SSTO and TSTO LOX Collection System Performances: Influence of LOX Plant Architecture”, Paper ICAS-96-3.8.3, presented at the 1996 International Council of the Aeronautical Sciences, Sorrento, Italy, 08–13 September 1996.
Holley, A.T., Wong, W.Y., Rowland, R.A., Meyers E.T., and Freese, R.A. (2012) “Combined Experimental and Modeling Pulsed Detonation Engine Combustor Performance Evaluation Technique”, JANNAF paper presented at the CS/APS/EPSS/PSHS Joint Subcommittee Meeting, Monterey CA 3–7 December 2012.
Jacob, D., Sachs, G. and Wagner, S. (Editors) (2005) “Basic Research and Technologies for Two-Stage-to-Orbit Vehicles”, Final Report of the Collaborative Research Centres 253, 255 and 259, Deutsche Forschungsgemeinschaft, Wiley-VCH Verlag, December 2005.
Jenkins, D.R. (2001) Space Shuttle: The History of the National Space Transportation System, The First 100 Missions, 3rd Edition, Midland Publishing, March 2001.
Jenkins, D.R. (2007) “X-15: Extending the Frontiers of Flight”, NASA SP-2007-562, NASA, 2007.
Johnson, M., Stevens, N. et al. (2014) For the Moon and Mars: N-1 – A Reference Guide to the Soviet Superbooster, 1st Edition, ARA Press, March 2014.
Kailasanath, K. (2002) “Recent Developments in the Research on Pulse Detonation Engines” (Invited), Paper AIAA-2002-0470, presented at the 40th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, 14–17 January 2002.
Kalmykov, G.P. et al. (2008) “LOX-Hydrocarbon Engines in Russia”, in Advanced Propulsion Systems and Technologies: Today to 2000, edited by C. Bruno and A.G. Accettura, AIAA Progress in Astronautics and Aeronautics Series, Vol. 223, AIAA, Reston, VA., Chapter 14, March 2008.
Kantrowitz, A. (1978) “Laser-Assisted Propulsion Research”, in: Radiation Energy Conversion in Space, ed. by K.W. Billman, AIAA Progress in Aeronautics and Astronautics Series, Vol. 61, p. 271.
Kingsbury, N.R. (1991) “Aerospace Plane Technology: Research and Development Efforts in Europe”, GAO/NSIAD-91-194, Report to the Chairman, Committee on Science, Space, and Technology, House of Representatives, United States General Accounting Office, July 1991.
Koelle, D.E. (1989) “On the Optimum Cruise Speed of a Hypersonic Aircraft”, IEEE Aerospace and Electronic Systems Magazine, Vol. 4, No. 5, May 1989, pp. 13–16.
Koelle, D.E., Sacher, P.W., and Grallert, H. (2007) “Deutsche Raketenflugzeuge und Raumtransporter-Projekte”, 1st Edition, Band 34, Die Deutsche Luftfahrt, Buchreihe über die Entwicklungsgeschichte der Deutschen Luftfahrttechnik, 2007.
Kroon, R.P. (1952) “Turbojet Performance Manual”, Engineering Department, Dept. A-1200, Westinghouse Electric Corporation, Aviation Gas Turbine Division, 1952
Kuczera, H. and Sacher, P.W. (2011) Reusable Space Transportation Systems, 1st Edition, Springer/Praxis Publisher, London, January 2011.
Lashin, A.I., Kovalevski, M.M., Romankov, O.N. and Tjurikov, E.V. (1993) “Combined Propulsion System for Advanced Multipurpose Aerospace Plane (ASP)”, Paper IAF-93-S.4.479, presented at the 44th International Astronautical Federation Congress, Graz, Austria, October 1993.
Lee, Y.-M., Czysz, P.A. and Bruno, C. (2002a) “Magnetohydrodynamic Energy Bypass Performance Analysis for Hypersonic Vehicles”, paper AIAA 2002-3571, presented at the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Meeting, Indianapolis, IN, 7–10 July 2002.
Lee, Y.-M., Czysz, P.A., Bruno, C. and Petley, D. (2002b) “Implementation of Magnetohydrodynamic Energy Bypass Process for Hypersonic Vehicle” Paper IECEC-20174, presented at the 37th AIAA/IEE/ASME/SAE/ANS/AIChE Intersociety Energy Conversion Engineering Conference, Washington DC, 28 July–01 August 2002.
Lee, Y.M., Nikolic-Tirkas, B., Tarrant, G.S., Balepin, V., Petley, D. and Czysz, P.A. (2003) “Vortex Tube Air Separation Applications for Air Collection Cycle Hypersonic Vehicles”, Paper AIAA-2003-374, presented at the 41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 06–09 January 2003.
Lee, Y.-M., Czysz, P.A., and Bruno, C. (2003) “Implementation of Magnetohydrodynamic Energy Bypass for Hypersonic Vehicles”, Paper IAC-03-S.5.07, presented at the 54th International Astronautical Congress, Bremen, 28 September–03 October 2003.
Legostaev, V.P. (1984) Private communication with P.A. Czysz, 38th International Astronautical Congress (IAF), Brighton, UK, 10–17 October 1984.
Leingang, J.L. (1991) Personal communication with P.A. Czysz, Dayton, OH, 1991.
Leingang, J.L., Maurice, L.Q. and Carreiro, L.R. (1992) “Space Launch Systems Using Collection and Storage”, Paper IAF 92-0664, presented at the 43rd Congress of the International Astronautical Federation, Washington, DC, 28 August–05 September 1992.
Lin, B.C. and Lineberry, J.T. (1995) “An Assessment of T-Layer MHD”, Paper AIAA 95-1933, presented at the 26th AIAA Plasmadynamics and Lasers Conference, San Diego, CA, 19–22 June 1995.
Lindley, C.A. (1965) “Performance of Air Breathing and Rocket Engines for Hypervelocity Aircraft”, in: Proceedings of the 4th International Council of the Aeronautical Sciences (ICAS) Congress, Paris, 1964, Spartan Books, Washington, DC, 1965, pp. 941–976.
Lo, R.E., Adirim, H., Pilz, N., Schildknecht, A. et al. (2005) “Acquisition and Evaluation of Cryo-Solid Propulsion (CSP); Final Report: Summary of Most Important Results”, Technical Report TR Nr.36/03-2005, Aerospace Institute (AI), Berlin, Final Report to the European Space Agency ESA ESTEC, Contract 16830/02/NL/CP, Noordwijk, The Netherlands, March 2005.
Lozino-Lozinskiy, G.E. and Bratukhin, A.G. (Editors) (1997) Aerospace Systems: Book of Technical Papers, 1st Edition, Publishing House of Moscow Aviation Institute, Moscow, 1997.
Lozino-Lozinskiy, G.E., Skorodelov, V.A. and Plokhikh, V.P. (1993) “International Reusable Aerospace System MAKS - Present State of the Art and Perspectives”, presented at the 5th AIAA/DGLR International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, 30 November–03 December 1993.
Maita, M., Ohkami Y., Yamanaka, T. and Mori T. (1990) “Conceptual Study of Space Plane Powered by Hypersonic Airbreathing Propulsion System”, Paper AIAA-90-5225, presented at the 2nd International Aerospace Planes Conference, Orlando, FL, 29–31 October 1990.
Maurice, L.Q., Leingang, J.L. and Carreiro, L.R. (1992) “The Benefits of In-Flight LOX Collection for Air Breathing Space Boosters”, AIAA paper, presented at the 4th International Aerospace Planes Conference, Orlando, FL, 01–04 December 1992.
Merlin, P.W. (2002) “Mach 3+ NASA/USAF YF-12 Flight Research, 1969-1979”, Monographs in Aerospace History #25, NASA SP-2001-4525, 2002.
Miki, Y., Taguchi, H. and Aoki, H. (1993) “Status and Future Planning of LACE Development”, Paper AIAA-93-5124, presented at the 5th International Aerospace Planes & Hypersonics Technology Conference, Munich, Germany, 30 November–03 December 1993.
Miller, J. (2001) The X-Planes - X-1 to X-45, 3rd Edition, Midland Publishing, Hinkley, UK, 2001.
Morring, F. (2016) “Dream Chaser Wins Spot in 2nd Round ISS Cargo Contract”, Aviation Week & Space Technology, 14 January 2016.
Mulready, D. (2001) Advanced Engine Development at Pratt & Whitney (The Inside Story of Eight Special Projects 1946-1971), SAE International, Warrendale, PA., 2001, ISBN: 0-76800664-3.
Myrabo, L.N. (1982) “A Concept for Light-Powered Flight”, Paper AIAA-78-698, presented at the 18th AIAA Joint Propulsion Conference, Cleveland, OH, 21–23 June 1982.
Myrabo, L.N. (1983) “Advanced Beamed-Energy and Field Propulsion Concepts”, NASA-CR-176108, BDM Corporation publication BDM/W-83-225-TR, Final Report for the California Institute of Technology and Jet Propulsion Laboratory under NASA contract NAS7-1000, Task Order RE-156, May 1983.
Myrabo, L.N. (2001) “World Record Flights of Beam-Riding Rocket Lightcraft: Demonstration of ‘Disruptive’ Propulsion Technology”, Paper AIAA-2001-3798, presented at the 37th AIAA Joint Propulsion Conference and Exhibit, Salt Lake City, UT, 08–11 July 2001.
Myrabo, L.N. et al. (1988) “Apollo Lightcraft Project”, NASA-CR-184749, Final Report, prepared for NASA/USRA Advanced Design Program, 4th Annual Summer Conference, Washington, DC, 13–17 June 1988.
Myrabo, L.N. and Lewis, J.S. (2009) Lightcraft Flight Handbook: LTI-20, 1st Edition, Apogee Books, May 2009.
Myrabo, L.N., Messit, D.G. and Mead, F.B. (1998) “Flight and Ground Tests of a Laser-Boosted Vehicle”, Paper AIAA-98-3735, presented at the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, OH, 13–15 July 1998.
Neufeld, M.J. (1995) The Rocket and the Reich – Peenemünde and the Coming of the Ballistic Missile Era, 1st Edition, The Free Press, 1995.
Nicholas, T.M.T., Narayanan, A.K. and Muthunayagam, A.E. (1996) “Mixing Pressure-Rise Parameter for Effect of Nozzle Geometry in Diffuser-Ejectors”, Journal of Propulsion and Power, Vol. 12, No. 2, 1996, pp. 431–433.
Norris, G. (2003) “Pulse Power”, Flight International, Vol. 163, No. 4887, 1–23 June 2003, pp. 50–52.
Norris, G. (2015) “Air-breathing Sabre Concept Gains Credibility”, Aviation week & Space Technology, 30 July 2015.
Nouse, H., Minoda, M., et al. (1988) “Conceptual Study of Turbo-Engines for Horizontal Take-Off and Landing Space Plane”, Paper IAF-88-253, presented at the 39th International Astronautical Federation Congress, October 1988.
Novichkov, N. (1990a) “Space Wings of Russia and the Ukraine”, Article in Magazine Echoes of the Planet/Aerospace, Moscow, September 1990.
Novichkov, N. (1990b) Private communication, 41st International Astronautical Federation Congress (IAF), Dresden, Germany, 06–12 October 1990.
Ogawara, A. and Nishiwaki, T. (1989) “The Cycle Evaluation of the Advanced LACE Performance”, Paper IAF-89-313, presented at the 40th International Astronautical Federation Congress, Malaga, Spain, October 1989.
Osborn, K. (2015) “AF Chief Scientist: Air Force Working on New Hypersonic Air Vehicle”, Defense Tech, 01 June 2015.
Parkinson, R.C. (1991) “The An-225/Interim HOTOL Launch Vehicle”, AIAA Paper AIAA-91-5006, presented at the 3rd AIAA International Aerospace Planes Conference, Orlando, Florida, December 1991.
Pegg, J., Hunt, L. and Petley, D.H. (1993) “Design of a Hypersonic Waverider-Derived Airplane”, Paper AIAA-93-0401, presented at the 31st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 11–14 January 1993.
Phipps, C.R. and Luke, J.R. (2007) “Laser Space Propulsion”, in: Laser Ablation and Its Applications, Springer, New York. Chapter 16, 2007.
Pirrello, C.J. and Czysz, P.A. (1970) “Hypersonic Research Facilities Study”, Volumes I–VI, National Aeronautics and Space Administration Contract NAS2-5458 by McDonnell Aircraft Company (MCAIR), NASA CR 114322-114331, October 1970.
Poggie, J., McLaughlin, T. and Leonov, S. (2016) “Plasma Aerodynamics: Current Status and Future Directions”, Journal AerospaceLab, AL 10-01, December 2015.
Rife, J.P. and Cantelon, P.L. (2010) “Speeds Up to Orbital’: A History of the William H. Avery Advanced Technology Development Laboratory”, John Hopkins APL Technical Digest, Vol. 28, Number 4, 2010, pp. 306–323.
Riggins, D.W. (1996) “Brayton Cycle Engine/Component Performance Assessment Using Energy and Thrust-based Methods”, Paper AIAA-1996-2922, presented at the 32nd AIAA Joint Propulsion Conference and Exhibit, Lake Buena Vista, FL, 01–03 July 1996.
Roed, A. (1972) “Development of the Saab-Scania Viggen”, Canadian Aeronautics and Space Journal, Vol. 18, June 1972, pp. 167–175.
Rudakov, A.S. and Balepin, V.V. (1991a) “Propulsion Systems with Air Precooling for Aerospaceplane”, SAE Technical Paper 911182, Society of Automotive Engineers, April 1991.
Rudakov, A.S., Gatin, R.Y., Dulepov, N.P., Koralnik, B.N., Harchevnikova, G.D. and Yugov, O.K. (1991b) “Analysis of Efficiency of Systems with Oxidizer Liquefaction and Accumulation for Improvement of Spaceplane Performance,” Paper IAF-91-270, presented at the 42nd International Astronautical Federation Congress, Montreal, Canada, October 1991.
Sänger, E. (1956) “Flight Mechanics of Photon Rockets”, Aero Digest, 1956, p. 68–73.
Schall, W.O., Eckel, H.A., and Bohn, W.L. (2007) “Laser Propulsion Thrusters for Space Transportation”, in: Laser Ablation and Its Applications, ed. by C.R. Phipps, Springer, New York, Chapter 17, 2007.
Scherrer, D. (1988) “Evaluation du Concept de Fusée-Statoréacteur Pour la Propulsion Hypersonique”, ONERA Activities 1988, ONERA, Paris, April 1988.
Schweikart, L. (1998) “The Hypersonic Revolution: Case Studies in the History of Hypersonic Technology; Volume III: The Quest for the Orbital Jet: The National Aero-Space Program (1983–1995)”, 2nd Printing, Volume III, Air Force History and Museum Program, 1998.
Scott, T. and Riggins, D.W. (2000) “Work Interaction in Quasi-One Dimensional Flows”, Journal of Propulsion & Power, Vol. 16, No. 6, pp. 1053–1059.
Smereczniak, P. (1996) “Electromagnetic Drag Reduction (EMDR) Program”, Contract F33657-96-D-2004-0002, Developed for Aeronautical Systems Center Planning Directorate (ASC/XR), 1996.
Stine, G.H. (1996) Halfwhere to Anywhere – Achieving America’s Destiny in Space, 1st Edition, M. Evans and Company, Inc., October 1996.
Stroup, K.E. and Pontez, R.W. (1968) “Advanced Ramjet Concepts – Volume 1: Ejector Ramjet Systems Demonstration”, Report AFAPLTR-67-118, US AF Contract AF33(615)-3734, The Marquardt Corporation Final Report, May 1968.
Sutton, G.P. and Biblarz, O. (2010) Rocket Propulsion Elements, 8th Edition, Wiley Publisher, New York, February 2010.
Swithenbank, J. (1967) “Hypersonic Airbreathing Propulsion”, Progress in Aerospace Sciences, Vol. 8, Pergamon Press, New York, 1967, pp. 229–294.
Swithenbank, J. (1984) Oral presentation on scramjet research at Sheffield University, May 1984.
Swithenbank, J. and Chigier, N.A. (1969) “Vortex Mixing for Supersonic Combustion”, XXI (International) Symposium on Combustion, The Combustion Institute, Pittsburgh, PA, 1969, pp. 1154–1162.
Szames, A. (2001) “Enquête sur une énigme: l’avion hypersonique Ajax”, Air et Cosmos, No. 1777, January 2001, pp. 22–24.
Tanatsugu, N., Inatani, Y, Makino, T. and Hiroki, T. (1987) “Analytical Study of Space Plane Powered by Air-Turbo Ramjet with Intake Air Cooler”, Paper IAF-87-264, presented at the International Astronautical Federation (IAF) Congress, Brighton, UK, October 1987.
Tasić, J. (2006) “The Name of Nikola Tesla in Belgrade: Following the Trail of Light”, BelGuest, Summer 2006.
Tesla, N. (2007) Nikola Tesla: Colorado Spring Notes, 1899–1900, 1st Edition, BN Publishing, June 2006.
Togawa, M., Aoki, T. et al. (1991) “A Concept of LACE for SSTO Space Plane”, AIAA Paper 91-5011, presented at the 3rd International Aerospace Planes and Hypersonics Technologies Conference, December 1991.
Townend, L. (1986) Oral presentation to NASP technical team on scramjet test in 1966, Hampshire, UK, April 1986.
Townend, L. and Vandenkerckhove, J. (1994) “External Afterburning and Shock-Confined Combustion in Supersonic Flow”, APECS-VDK 001/94, ESA contract 120285, European Space Agency, 1994.
Tretyakov, P. (1995) “Supersonic Flow Around Axisymmetric Bodies with External Supply of Mass and Energy”, Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia, 1995.
Tretyakov, P.K., Golovitchev, V.I. and Bruno, C. (1995) “Experimental and Numerical Study of Counterflow Jet Flame Stabilization in a Supersonic Air Stream”, paper presented at the XII International Society of Air Breathing Engines (ISABE), Melbourne, Australia, 10–15 September 1995.
Vandenkerckhove, J.A. (1986) Personal communication with P.A. Czysz about Von Kármán at CalTech, March 1986.
Vandenkerckhove, J.A. (1991) “A First Assessment of Scramjet-Propelled Single-Stage-to-Orbit (SSTO) Vehicles”, WLC Phase 5, WP 260, Chapter 1, VDK System S.A., Brussels, Belgium, February 1991.
Vandenkerckhove, J.A. (1992a) “A Peep Beyond SSTO Mass Marginality”, Paper IAF-92-0656, presented at the 43rd International Astronautical Federation Congress, 28 August–05 September 1992.
Vandenkerckhove, J.A. (1992b) “SSTO Configuration Assessment”, Chapter 2, Revision 1, VDK System S.A., WLC Phase 5, WP 260, Brussels, Belgium, August 1992.
Vandenkerckhove, J.A. (1993a) “HYPERJET Mk #3, A Rocket-Derived Combined Engine”, VDK System Report, April 1993.
Vandenkerckhove, J.A. (1993b) “Comparison Between Ejector-Ramjets & Turbo-Ramjets for T.S.T.O. Propulsion”, Paper AIAA-93-5095, presented at the 5th International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, 30 November–03 December 1993.
Weeden, B. (2010) “X-37B Orbital Test Vehicle Fact Sheet”, Secure World Foundation, 23 November 2010.
Werrell, K.P. (1985) The Evolution of the Cruise Missile, 1st Edition, Air University Press, September 1985.
Wu, Y., Ma, F. and Yang, V. (2003) “System Performance and Thermodynamic Cycle Analysis of Air-Breathing Pulse Detonation Engines”, Journal of Propulsion and Power, Vol. 19, No. 4, July–August 2003.
Yabe, T. and Uchida, S. (2007) “Laser Propulsion”, in: Laser Ablation and Its Applications, ed. by C.R. Phipps and Luke, J.R., Springer, New York, Chapter 18, 2007.
Yamanaka, T. (2000) “Innovative Breakthroughs to a Reusable STS”, private communication with P.A. Czysz, 2000.
Yamanaka, T. (2004) “Fundamentals of Airbreathing Rocket Combined Cycle (ARCC) Engine and Design of an ARCC Engine Powered Single-Stage-To-Orbit (SSTO) Vehicle”, Beyond the Atmosphere CDROM, July 2004.
Yugov, O. K., et al. (1989) “Optimal Control Programs for Airbreathing Propulsion System or Single-Stage-to-Orbit Vehicles”, Paper IAF-89-308, presented at the 40th IAF Congress, International Astronautical Federation, Malaga, Spain, October 1989.
Yugov, O.K., Dulepov, N.P. and Harchenvnikova, G.D. (1990) “The Analysis of Hypersonic and Combined Cycle Engines in the Propulsion System of the SSTO Vehicles”, presented at the 41st IAF (International Astronautical Federation) Congress, Dresden, Germany, October 1990.
Zagainov, G.I. and Plokhikh, V.P. (1991) “USSR Aerospace Plane Program”, Paper AIAA-91-5103, presented at the 3rd International Aerospace Planes and Hypersonics Technologies Conference, Orlando, FL, 03–05 December 1991.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2018 Springer-Verlag GmbH Germany
About this chapter
Cite this chapter
Czysz, P.A., Bruno, C., Chudoba, B. (2018). Commercial Near-Earth Launcher: Propulsion Choices. In: Future Spacecraft Propulsion Systems and Integration. Springer Praxis Books(). Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-54744-1_4
Download citation
DOI: https://doi.org/10.1007/978-3-662-54744-1_4
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-662-54742-7
Online ISBN: 978-3-662-54744-1
eBook Packages: EngineeringEngineering (R0)