X-43A vehicle design and manufacture

A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 2, Issue , 2005, Pages 1220-1228

  Harsha, Philip T ^a   Keel, Lowell C ^a   Castrogiovanni, Anthony ^a   Sherrill, Robert T ^b  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT ENGINES; HYPERSONIC AERODYNAMICS; PROPULSION; RESEARCH; SENSORS;

AIRBREATHING; INTEGRATED SENSORS; SUBSYSTEMS; VEHICLE DESIGN;

FLIGHT DYNAMICS;

EID: 29044438073     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-3334     Document Type: Conference Paper

References (12)

1. Hunt, J., and Eiswirth, E., "NASA's Dual-Fuel Airbreathing Hypersonic Vehicle Study," AIAA 96-4591.
2. Bahm, C., et al, "X-43A Guidance, Navigation and Control Challenges," AIAA-2005-3275.
3. Rock, K., et al, "Hyper-X Mach 7 Scramjet Ground Test to Flight Comparison," AIAA-2005-3321.
4. Ferlemann, S., "Hyper-X Mach 7 Scramjet Preflight Predictions vs. Flight Results," AIAA-2005-3322.
5. Corpening, G., et al, "A Chief Engineer's View of NASA's X-43A Scramjet Flight Test," AIAA-2005-3332.
6. Blocker, W., and Reubush, D., "X-43A Stage Separation System-A Flight Data Evaluation," AIAA-2005-3335.
7. Marshall, L., et al, "X-43A Flight 3 Preparation and Results," AIAA-2005-3336.
8. Grindle, T., et al, "Hyper-X Fluid/Environmental Systems Performance on Flights 1, 2, and 3," AIAA-2005-3337.
9. Rogers, R., et al, "Scramjet Development and Evaluation Tests for the Hyper-X Mach 10 Flight," AIAA-2005-3351.
10. Ferlemann, S., "Hyper-X Mach 10 Scramjet Preflight Predictions vs. Flight Data," AIAA-2005-3352.
11. Engelund, W., "Hyper-X/X-43A Aerodynamic Results from the Mach 7 and Mach 10 Scramjet Flight Tests," AIAA-2005-3405.
12. Leonard, C., et al. "Hyper-X Hot Structures Design and Comparison with Flight Data," AIAA-2005-3348.