Probabilistic analysis of turbine-based combined cycle space vehicles

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2004, Pages

  Villeneuve, Frederic J ^a   Waters, Mark H ^a,b   Mavris, Dimitri N ^a  

^a Georgia Institute of Technology   (United States)

^b GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR-BREATHING PROPULSION; COMBINED CYCLE; COMBINED-CYCLE PROPULSION SYSTEMS; DESIGN PROCESS; DESIGN SPACES; ECONOMIC PERFORMANCE; LEGACY CODE; MULTI-STAGE; PHYSICS-BASED MODELING; PROBABILISTIC ANALYSIS; SPACE ANALYSIS; SPACE VEHICLES; SYNTHESIS PROCEDURE; TWO-STAGE-TO-ORBIT VEHICLES;

CONCEPTUAL DESIGN; PROPULSION; TURBINES;

VEHICLES;

EID: 77957848241     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Heppenheimer, T.A., The history of the space shuttle, Smithsonian Inst. Press, Washington, 2002,478 p.
2. rd Edition, Reston VA, AIAA 1999, 923 p.
3. Humble, R.W., Henry, G.N., Larson, W.J., Space Propulsion Analysis and Design, McGraw Hill, 1995, 748 p.
4. Mahadevan S. and Smith, N. L. "System Risk Assessment and Allocation in Conceptual Design"..NASA/CR-2003-212162, May 2003.
5. Bryson, A.E., Desai, M.N., and Hoffman, W.C. "Energy-State Approximation in Performance Optimization of Supersonic Aircraft," Journal of Aircraft, Vol. 6, No. 6,. 1969, pp. 481-488.
6. Thomson, W.T., Introduction to Spacecraft dynamics Dover Publications, 1986, 352 p.
7. William, L.J., "Estimated Aerodynamics of All-Body Hypersonic Aircraft Configurations", NASA Report TM X-2091, March 1971.
8. Van Dyke, M.D., "The Slender Elliptic Cone as a Model for Nonlinear Supersonic Flow Theory," Journal of Fluid Mechanics, Volume 1, May 1956, pp. 1-15.
9. th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 15-19 De. 2003, Norfolk, VA, AIAA 2003-7042.
10. Mahoney, J.J, Inlets for Supersonic Missiles AIAA Educational Series, 1990, 237 p.
11. Apel, G.F., Crim, H.S., "Estimated Performance of a Mach 4.0 Hydrogen Fueled Stoichiometric Turbojet Engine", Pratt & Whiney Aircraft, 1967.
12. nd ed., Addison Wesley, Cambridge, 1992.
13. Harloff, G.J., Berkowitz, B.M., " HASA, Hypersonic Analysis Code, NAS3-24105, Nov. 1988.
14. Eloret Corp, "NASA/Air Force Cost Model" NAS2-00062.