Dual-fuel vehicle airframe and engine structural integration

Space Plane and Hypersonic Systems and Technology Conference

Volumn 1 PartF, Issue , 1996, Pages

  Weirich, Tony L ^a   Fogarty, William ^a   Dry, Kevin ^a   Iqbal, Ahsan ^a   Moses, Paul L ^b  

^a BOEING COMPANY   (United States)

^b Lockheed Martin Engineering and Sciences   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; AUTOMOBILE FUEL TANKS; CRYOGENICS; FUELS; GRAPHITE; HYPERSONIC VEHICLES; RAMJET ENGINES; STRUCTURAL FRAMES; SUPERSONIC AIRCRAFT; THERMAL INSULATION;

AIRFRAME STRUCTURES; CROSS SECTIONAL AREA; CRYOGENIC FUEL TANKS; MISSION REQUIREMENTS; PERFORMANCE ISSUES; STRUCTURAL INTEGRATION; THERMAL PROTECTION; THERMALLY PROTECTED;

DUAL FUEL ENGINES;

EID: 85072042373     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-4594     Document Type: Conference Paper

References (4)

1. 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, Paper No. 96-2894,32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Lake Buena Vista, FZ, July, 1996.
2. Droegkamp, Mark, and Kevin Dry, ADVISOR Users Guide, Version 3.0, Release 96.2, McDonnell Douglas, St. Louis, MO, September 1996.
3. Ngo, D. A., Koshiba, D. A., and Moses, P. L., Hypersonic Vehicle Structural Weight Prediction Using Parametric Modeling, Finite Element Modeling, and Structural Optimization, Paper No. 93-1397,34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, La Jolla, CA, April, 1993.
4. Alberico, J.F., Espinosa, A.M., and Hopping, B.M., HOLIST User’s Guide, McDonnell Douglas, St. Louis, MO, September 1994.