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Airbreathing Hypersonic Vision-Operational-Vehicles Design Matrix
Technical Paper
1999-01-5515
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
This paper presents the status of the airbreathing hypersonic airplane and space-access vision-operational-vehicle design matrix, with emphasis on horizontal takeoff and landing systems being studied at Langley; it reflects the synergies and issues, and indicates the thrust of the effort to resolve the design matrix including Mach 5 to 10 airplanes with global-reach potential, pop-up and dual-role transatmospheric vehicles and airbreathing launch systems. The convergence of several critical systems/technologies across the vehicle matrix is indicated. This is particularly true for the low speed propulsion system for large unassisted horizontal takeoff vehicles which favor turbines and/or perhaps pulse detonation engines that do not require LOX which imposes loading concerns and mission flexibility restraints.
Authors
Citation
Hunt, J., Pegg, R., and Petley, D., "Airbreathing Hypersonic Vision-Operational-Vehicles Design Matrix," SAE Technical Paper 1999-01-5515, 1999, https://doi.org/10.4271/1999-01-5515.Also In
References
- Hunt, J.L. Lockwood, M.K. Petley, D.H. Pegg, R.J. Hypersonic Airbreathing Vehicle Visions and Enhancing Technologies. Space Technology and Applications International Forum AIP Conference Proceedings 387 Albuquerque, NM 1997
- Rausch, V.L. McClinton, C.R. Crawford, J.L. Hyper-X: Flight Validation of Hypersonic Airbreathing Technology ISABE 97-7024
- Hunt, J.L. Couch, L.M. Beyond Hyper-X. ASCE Space í98 Albuquerque, NM April 26-30 1998
- Pegg, R.J. Hunt, J.L. Petley, D.H. Burkardt, L. Stevens, D.R. Moses, P.L. Pinckney, S.Z. Kabis, H.Z. Spoth, K.A. Dziedzic, W.M. Kreis, R.I. Martin, J.G. Barnhart, P.J. Design of a Hypersonic Waverider-Derived Airplane AIAA 93-0401
- Hunt, J.L. Eiswirth, E.A. NASA’s Dual-Fuel Airbreathing Hypersonic Vehicle Study AIAA 96 - 4591
- Bogar, T.J. Eiswirth, E.A. Couch, L.M. Hunt, J.L. McClinton, C.R. Conceptual Design of a Mach 10, Global Reach Reconnaissance Aircraft AIAA 96-2894
- Hunt, J.L. Laruelle, G. Wagner, A. Systems Challenges for Hypersonic Vehicles AGARD Paper C37 Ecole Polytechnique Palaiseau Paris, France 1997
- Saeks, R. Cox, C.J. Pap, R.M. LoFLYTE“!: A Neurocontrols Testbed AIAA 97-0085
- Takashima, N. Lewis, M.J. Lockwood, M.K. Bogar, T. Johnson, D. Waverider Configuration Development for the Dual Fuel Vehicle AIAA 96-4593
- Hunt, James L. Rausch, Vincent L. Airbreathing Hypersonic Systems Focus at NASA Langley Research Center AIAA 98-1641
- Access to Space Study: Summary Report; Office of Space Systems Development, NASA Headquarters Jan. 1994.
- Bekey, I. Powell, R. Austin, R. NASA Studies Access to Space Aerospace America May 1994
- Hunt, J. L. Airbreathing/Rocket Single-Stage-to- Orbit Design Matrix AIAA 95-6011
- Kothari, A.P. Tarpley, C. et al. Hypersonic Vehicle Design Using Inward Turning Flowfields AIAA 96-2552
- Keirsey, J.L. A Study of the Aerodynamics of Scramjet Engine Inlets The Johns Hopkins University Applied Physics Laboratory, TG-732, Sep. 1965
- Jackson, L.R. An Accelerator Airplane Concept for Single-Stage-to-Orbit Flight NASA TM 101563 Sept. 1989
- Hawkins, R.W. Richardson, P.F. Design and Off-Design Performance Analysis of a Maximum Compression/ Minimum Drag Hypersonic Forebody AIAA 91-3179
- Balepin, V. Cozzog, P. Marta, M. Vanderkerckhove P. Assessment of SSTO Performance with In-Flight LOX Collection AIAA 95-6047
- Bussing, R.R.A. Pappus, G. An Introduction to Pulse Detonation Engines AIAA 94-0263
- Gregory, T. Bowles, J. Ardema, M. Two Stage to Orbit Airbreathing and Rocket System for Low Risk, Affordable Access to Space SAE 941168
- Yi, A.C. Reusable SSTO/TSTO Launch System Using Air Liquefaction Enrichment System (ALES Propulsion) NASA CR 191156 1-5 June 1993
- Lockwood, M.K. Hunt, J.L. Kabis, H.Z. Moses, P.L. Pao, J.L. Yarrington, P.W. Collier, C. Design and Analysis of Two-Stage-to-Orbit Airbreathing Hypersonic Vehicle Concept AIAA 96-2890
- Scuderi, G.F. Orton, G.F. Hunt, J.L. Mach 10 Cruise/Space Access Vehicle Definition AIAA98-1584