Airbreathing hypersonic systems focus at NASA Langley Research Center

8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1998, Pages 1-16

  Hunt, James L ^a   Rausch, Vincent L ^b  

^a Manager of Systems Analysis Office   (United States)

^b NASA LaRC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; NASA; SPACECRAFT; VEHICLES;

AIR BREATHING; DESIGN MATRIX; HYPERSONIC SYSTEMS; NASA LANGLEY RESEARCH CENTER; SPACE ACCESS VEHICLES; TECHNOLOGY MATURATION;

DESIGN;

EID: 84983189129     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (23)

1. Hunt, J.L.; Lockwood, M.K.; Petley, D.H.; and Pegg, R.J.: Hypersonic Airbreathing Vehicle Visions and Enhancing Technologies. Space Technology and Applications International Forum. AIP Conference Proceedings 387, Albuquerque, MM, 1997.
2. Rausch, V.L.; McClinton, C.R.; and Crawford, J.L.: Hyper-X: Flight Validation of Hypersonic Airbreathing Technology. ISABE 97-7024, Chattanooga, TN, Sep. 1997.
3. Hunt, J.L.; and Couch, L.M.: Beyond Hyper-X. ASCE Space '98, Albuquerque, MM, April 26-30, 1998.
4. 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.; and Barnhart, P.J.: Design of a Hypersonic Waverider-Derived Airplane. ALAA 93-0401, Reno, NV, Jan. 11-14, 1993.
5. Hunt, J.L.; and Eiswirth, E.A.: NASA's Dual-Fuel Airbreathing Hypersonic Vehicle Study. AIAA 96-4591, Norfolk, VA, Nov. 18-22, 1996.
6. Bogar, T.J.; Eiswirth, E.A.; Couch, L.M.; Hunt, J.L.; and McClinton, C.R.: Conceptual Design of a Mach 10, Global Reach Reconnaissance Aircraft. AIAA 96-2894, Lake Buena Vista, FL, July 1-3,1996
7. Hunt, J.L.; Laruelle, G.; and Wagner, A.: Systems Challenges for Hypersonic Vehicles. AGARD Paper C37, Ecole Polytechnique Palaiseau, Paris, France, April 14-16,1997.
8. th Aerospace Sciences Meeting & Exhibit, Reno, Nevada, January 1997.
9. Takashima, N.; Lewis, M.J.; Lockwood, M.K.; Bogar, T.; and Johnson, D.: Waverider Configuration Development for the Dual Fuel Vehicle. AIAA 96-4593.
10. Bogar, T.J.; Alberico, J.F.; Johnson, D.B.; Espinosa, A.M.; and Lockwood, M.K.: Dual-Fuel Lifting Body Configuration Development. AIAA 96-4592, Norfolk, VA, Nov. 18-22,1996.
11. Access to Space Study: Summary Report; Office of Space Systems Development, NASA Headquarters, Jan. 1994.
12. Bekey, L; Powell, R.; and Austin, R.: NASA Studies Access to Space. Aerospace America, May 1994.
13. Hunt, J. L.: Airbreathing/Rocket Single-Stage-to-Orbit Design Matrix. AIAA 95-6011, Chattanooga, TN, April 3-7,1995.
14. Kothari, A.P.; Tarpley, C. et al.: Hypersonic Vehicle Design Using Inward Turning Flowfields. AIAA 96-2552,1996.
15. Keirsey, J.L.: A Study of the Aerodynamics of Scramjet Engine Inlets. The Johns Hopkins University Applied Physics Laboratory, TG-732, Sep. 1965.
16. Jackson, L.R.: An Accelerator Airplane Concept for Single-Stage-to-Orbit Flight. NASA TM 101563, Sep. 1989.
17. Hawkins, R.W.; and Richardson, P.P.: Design and Off-Design Performance Analysis of a Maximum Compression/ Minimum Drag Hypersonic Forebody. AIAA 91-3179, Aircraft Design Systems and Operations Meeting, Baltimore, MD, Sep. 23-25,1991.
18. Balepin, V.; Cozzog, P.; Marta, M.; and Vanderkerckhove, M: Assessment of SSTO Performance with In-Flight LOX Collection. AIAA 95-6047,1995.
19. Bussing, R.R.A.; and Pappus, G.: An Introduction to Pulse Detonation Engines. AIAA 94-0263,1994.
20. Gregory, T.; Bowles, J.; and Ardema, M.: Two Stage to Orbit Airbreathing and Rocket System for Low Risk, Affordable Access to Space. SAE 941168, SAE 1994 Aerospace Atlantic Conference and Exposition, Dayton, Ohio, April 19, 1994.
21. Yi, A.C.: Reusable SSTO/TSTO Launch System Using Air Liquefaction Enrichment System (ALES Propulsion). NASA CR 191156, Volumes 1-5, June 1993.
22. Lockwood, M.K.; Hunt, J.L.; Kabis, H.Z.; Moses, P.L.; Pao, J.L.; Yarrington, P.W.; and Collier, C.: Design and Analysis of Two-Stage-to-Orbit Airbreathing Hypersonic Vehicle Concept. AIAA 96-2890, Lake Buena Vista, FL, July 1-3 1996.
23. Scuderi, G.F., Orton, G.F., and Hunt, J.L.: Mach 10 Cruise/Space Access Vehicle Definition. AIAA 98-1584, AIAA 8th International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk, VA, Apr. 1998