1 |
Korte, J. J., Salas, A. O., Dunn, H. J., Alex, N. M., Follet, W. W., Oreint, G. E., and Hadid, A., H., "Multidisciplinary Approach to Aerospike nozzle design", NASA-TM- 110326.
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2 |
George P. Shutton& Oscar Biblarz, 2000, Rocket Propulsion Elements, Wiley India Pvt. Ltd. Seventh Edition, p. 33, 68-80.
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3 |
Paul V. Tartabini, Roger A. Lepsch, Korte, J. J., and Kathryn E. Wurster, 2000, "A Multidisciplinary Performance Analysis of A Lifting-Body Single-Stageto- Orbit Vehicle", AIAA-2000-1045.
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4 |
Verma, S. B., 2009, "Study of Restricted Shock Separation Phenomenon in a Thrust Optimized Parabolic Nozzle", J. Propulsion and Power.
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5 |
Shannon D. Eilers, Matthew D. Wilson, and Stephen A. Whitmore, 2010, "Analytical and Experimental Evaluation of Aerodynamic Thrust Vectoring on an Aerospike Nozzle", 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. & Exhibit, Nashville, TN.
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6 |
Korte, J. J., 2000, "Parametric Model of an Aerospike Rocket Engine", AIAA-2000-1044.
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