-
4
-
-
84897703424
-
Airbreathing, Hypersonic Vision-Operational-Vehicle Design Matrix
-
SAE-1999-01-5515, Presented 1999, San Francisco, CA, Oct. 19-21
-
Hunt, J.L.; Pegg, R.J.; and Petley, D.H.: Airbreathing, Hypersonic Vision-Operational-Vehicle Design Matrix. SAE-1999-01-5515, Presented 1999 World Aviation Congress and Exposition, San Francisco, CA, Oct. 19-21,1999.
-
(1999)
World Aviation Congress and Exposition
-
-
Hunt, J.L.1
Pegg, R.J.2
Petley, D.H.3
-
5
-
-
0004289309
-
-
AIAA Education Series. AIAA, Inc., Washington, D.C., USA
-
Heiser, William H. and Pratt, Davis T.: Hypersonic Airbreathing Propulsion. AIAA Education Series. AIAA, Inc., Washington, D.C., USA. 1994.
-
(1994)
Hypersonic Airbreathing Propulsion
-
-
Heiser, W.H.1
Pratt, D.T.2
-
6
-
-
0005419514
-
-
Appendix A. A Lexicon for Combined-Cycle Hypersonic Propulsion Systems. Society of Automotive Engineers, Inc., Compiled and Edited by William J. D. Escher
-
"The Synerjet Engine. Airbreathing!Rocket Combined-Cycle Propulsion for Tomorrow's Space Transports," Appendix A. A Lexicon for Combined-Cycle Hypersonic Propulsion Systems. Society of Automotive Engineers, Inc., Compiled and Edited by William J. D. Escher., 1997.
-
(1997)
The Synerjet Engine. Airbreathing!Rocket Combined-Cycle Propulsion for Tomorrow's Space Transports
-
-
-
12
-
-
0016926901
-
Thermal-Structural Design/Analysis of an Airframe-Integrated Hydrogen-Cooled Scramjet
-
March
-
Wieting, A.R. and Guy, R.W.: Thermal-Structural Design/Analysis of an Airframe-Integrated Hydrogen-Cooled Scramjet. Journal Aircraft, Vol. 1, No 3, March 1976, pp. 192-197.
-
(1976)
Journal Aircraft
, vol.1
, Issue.3
, pp. 192-197
-
-
Wieting, A.R.1
Guy, R.W.2
-
13
-
-
84983189864
-
Comparative How Path Analysis and Design Assessment of an Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine at a Mach Number of 6.5
-
Presented. Norfolk, Va. AIAA Paper 96-4571, Nov
-
C. McClinton; A. Roudakov; V. Semenov and V. Kopehenov: Comparative How Path Analysis and Design Assessment of an Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine at a Mach Number of 6.5. Presented 7th International Spaceplanes and Hypersonic Systems and Technology Conference. Norfolk, Va. AIAA Paper 96-4571, Nov. 1996.
-
(1996)
7th International Spaceplanes and Hypersonic Systems and Technology Conference
-
-
McClinton, C.1
Roudakov, A.2
Semenov, V.3
Kopehenov, V.4
-
15
-
-
84983140094
-
Numerical Analysis of Convection/Transpiration Cooling
-
Presented. Norfolk, Va. AIAA, Nov
-
Glass, D.E.; Dilley, A.D.; and Kelly, H.N.: Numerical Analysis of Convection/Transpiration Cooling. Presented 7th International Spaceplanes and Hypersonic Systems and Technology Conference. Norfolk, Va. AIAA, Nov. 1999.
-
(1999)
7th International Spaceplanes and Hypersonic Systems and Technology Conference
-
-
Glass, D.E.1
Dilley, A.D.2
Kelly, H.N.3
-
17
-
-
84983177748
-
Composite Cryogenic Tanks and Primary Structures for Reusable Launch Vehicles
-
Oct. 19-22
-
Scotti, Stephen; Sawyer, Wayne; Johnson, Theodore; Rivers, Kevin; and Smith, Russell: Composite Cryogenic Tanks and Primary Structures for Reusable Launch Vehicles. 1998 National Space and Missile Materials Symposium, Oct. 19-22,1998.
-
(1998)
1998 National Space and Missile Materials Symposium
-
-
Scotti, S.1
Sawyer, W.2
Johnson, T.3
Rivers, K.4
Smith, R.5
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