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Current Aerocapture Technical References |
Aerocapture Assist |
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AIAA-2003-4655 Trailing Ballute Aerocapture: Concept and Feasibility Assessment |
AIAA-2003-4952 Preliminary Aerothermodynamics of Titan Aerocapture Aeroshell |
AIAA-2003-4951 Aerocapture Simulation and Performance for the Titan Explorer Mission |
AIAA-2003-4956 Planetary Probe Mass Estimation Tool Development and its Application to Titan Aerocapture |
AIAA-2003-4799 Titan Aerocapture Systems Analysis |
AIAA-2003-4804 Guidance Algorithms for Aerocapture at Titan |
AIAA-2003-4955 Structural Design of the Titan Aerocapture Mission |
AIAA-2003-4953 An Analysis of the Radiative Heating Environment for Aerocapture at Titan |
AIAA-2003-4954 Thermal Protection Concepts and Issues for Aerocapture at Titan |
AIAA-2004-0484 The Impact of Flowfield-Radiation Coupling on Aeroheating for Titan Aerocapture |
AIAA-2004-0486 Aeroheating Analysis for the Afterbody of a Titan Probe |
Comparison of Methods to Compute High-Temperature Gas Viscosity |
Collision Integrals for Ion-Neutral Interactions of Nitrogen and Oxygen |
AIAA-2004-2456 Analysis of Afterbody Heating Rates on the Apollo Command Modules, Part 1: AS-202 |
AIAA-2004-2469 N2-CH4-AR Chemical Kinetic Model for Simulations of Atmospheric Entry to Titan |
Lemmerman, L., Wercinski, P., "Small Neptune Orbiter Using Aerocapture," Space Technology and Applications International Forum, (STAIF-97), Albuquerque, NM, Jan. 1997 |
http://www.hq.nasa.gov/office/codez/plans /SSE00plan.pd |
Kos, L. et. al., "In-space Integrated Space Transportation Activity - Neptune Orbiter Mission Briefing," NASA Marshall Space Flight Center, April 2001 |
Tauber, M., Wercinski, P., Henline, W., Paterson, J., and Yang, L., "Uranus and Neptune Atmospheric Entry Probe Study," Journal of Spacecraft and Rockets, Vol. 31, No. 5, pp. 799-805, Sept-Oct., 1994 |
Lasher, L., Wilson, K. and Greif, R., "Radiation From an Isothermal Hydrogen Plasma at Temperatures Up To 40,000 K," Lockheed Palo Alto Research Laboratory 6-76-66-17 Revised July 1967 |
Nelson, F. and Goulard, R., "Equilibrium Radiation From Isothermal Hydrogen-Helium Plasmas," Journal of Quantitative Spectroscopy and Radiative Transfer, Vol. 8, 1968, pp. 1351-1372 |
Tauber, M. and Wakefield, R., "Heating Environment and Protection During Jupiter Entry," Journal of Spacecraft and Rockets, Vol. 8, No. 6, June 1971, pp. 630-636. |
Marvin, J. and Pope, R., "Laminar Convective Heating and Ablation in the Mars Atmosphere," AIAA Journal, Vol. 5, No. 2, 1967, pp. 240-248. |
Wright, M. J., Candler, G. V., and Bose, D., "A Data-Parallel Line Relaxation Method for the Navier-Stokes Equations," AIAA Journal, Vol. 36, No. 9, 1998, pp. 1603-1609. |
Olynick, D. R., Henline, W. D., Hartung-Chambers, L., and Candler, G. V., "Comparisons of Coupled Radiative Navier-Stokes Flow Solutions with the Project Fire II Flight Data," AIAA Paper No. 94-1955, June 1994. |
MacCormack, R.W. and Candler, G.V., "The Solution of the Navier-Stokes Equations Using Gauss-Seidel Line Relaxation," Computers and Fluids, Vol. 17, No. 1, 1989, pp. 135-150. |
Yee, H.C., "A Class of High-Resolution Explicit and Implicit Shock Capturing Methods," NASA TM 101088, 1989. |
Olejniczak, J. and Fletcher, D.G., "An Experimental and Computational Study of the Freestream Conditions in an Arc-Jet Facility," AIAA Paper No. 2000-2567, June 2000. |
Wright, M. J., Sinha, K., Olejniczak, J., Candler, G. V., Magruder, T. D., and Smits, A. J., "Numerical and Experimental Investigation of Double-Cone Shock Interactions," AIAA Journal, Vol. 38, No. 12, 2000, pp. 2268-2276. |
Wright, M. J., Loomis, M., and Papadopoulos, P., "Aerothermal Analysis of the Project Fire II Afterbody Flow," AIAA Paper No. 2001-3065, June 2001. |
Baulch, D.L., et. al., "Evaluated Kinetic Data for Combustion Modeling," Journal of Physical and Chemical Reference Data, Vol. 21, No. 3, 1992, pp. 411. |
Chen, Y.-K. and Milos, F., "Implicit Ablation and Thermal Response Program for Spacecraft Heatshield Analysis", Journal of Spacecraft and Rockets, Vol. 36, No. 3, May-June 1999, pp 475-483. |
Laub, B. and Beck, R. A. S., "Development of Baseline Response Model for Carbon Phenolic", Contract No. GS-23F-010K, ITT Aerotherm, Mountain View, CA 94043, Oct. 2000. |
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