Aerocapture Systems Analysis for a Titan Mission
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Jeffery L. Hall | Glenn A. Hrinda | Brett R. Starr | M. Lockwood | R. Bailey | K. Edquist | B. Hollis | T. Spilker | M. Noca | N. O'Kongo
[1] F. R. Riddell,et al. Theory of Stagnation Point Heat Transfer in Dissociated Air , 1958 .
[2] W. Nicolet. Advanced methods for calculating radiation transport in ablation-product contaminated boundary layers , 1970 .
[3] K. Sutton,et al. A general stagnation-point convective heating equation for arbitrary gas mixtures , 1971 .
[4] R. C. Ried,et al. Radiative heating to the Apollo command module: Engineering prediction and flight measurement , 1972 .
[5] Lewis P. Leibowitz,et al. Ionizational Nonequilibrium Heating During Outer Planetary Entries , 1976 .
[6] G. L. Brauer,et al. Capabilities and applications of the Program to Optimize Simulated Trajectories (POST). Program summary document , 1977 .
[7] J. C. Harpold,et al. Shuttle entry guidance , 1978 .
[8] C. Park. Radiation enhancement by nonequilibrium during flight through the Titan atmosphere , 1982 .
[9] H. C. Yee,et al. On symmetric and upwind TVD schemes , 1985 .
[10] J. D. Gamble,et al. A simplified guidance algorithm for lifting aeroassist orbital transfer vehicles , 1985 .
[11] G. M. Keating,et al. The Venus international reference atmosphere , 1986 .
[12] Chul Park,et al. Assessment of two-temperature kinetic model for ionizing air , 1987 .
[13] H. C. Yee,et al. A class of high resolution explicit and implicit shock-capturing methods , 1989 .
[14] Chul Park,et al. A review of reaction rates in high temperature air , 1989 .
[15] Graham V. Candler,et al. The solution of the Navier-Stokes equations using Gauss-Seidel line relaxation , 1989 .
[16] Ellis E. Whiting,et al. Titan atmospheric composition by hypervelocity shock-layer analysis , 1989 .
[17] P. Gnoffo. An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows , 1990 .
[18] Determination of the radiative emission of a hypersonic flow simulating the Cassini-Titan atmospheric entry probe environment , 1990 .
[19] D. Bershader,et al. Studies of radiative emission from the simulated shock layer of the Huygens probe , 1992 .
[20] C. Laux,et al. Optical Diagnostics and Radiative Emission of Air Plasmas , 1993 .
[21] R. A. Thompson,et al. The addition of algebraic turbulence modeling to program LAURA , 1993 .
[22] C. Lin,et al. Coupled Radiation Effects in Thermochemical Nonequilibrium Shock-Capturing Flowfield Calculations , 1994 .
[23] Lin Hartung Chambers,et al. Predicting radiative heat transfer in thermochemical nonequilibrium flow fields. Theory and user's manual for the LORAN code , 1994 .
[24] Gilles Taquin,et al. Huygens Probe Radiative Environment , 1995 .
[25] O. Talagrand,et al. Numerical simulation of the general circulation of the atmosphere of Titan. , 1995, Icarus.
[26] C. Justus,et al. The NASA/MSFC Global Reference Atmospheric Model: 1999 Version (GRAM-99) , 1995 .
[27] Cheatwood F. McNeil,et al. User''s Manual for the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA) , 1996 .
[28] James O. Arnold,et al. NEQAIR96,Nonequilibrium and Equilibrium Radiative Transport and Spectra Program: User's Manual , 1996 .
[29] HUYGENS probe aerothermodynamics , 1997 .
[30] Andrew Wilson. Huygens : science, payload and mission , 1997 .
[31] P. Roe. Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes , 1997 .
[32] G. Candler,et al. Data-Parallel Line Relaxation Method for the Navier -Stokes Equations , 1998 .
[33] Craig S. Collier,et al. Design Optimization Using HyperSizer , 1998 .
[34] Gerald D. Walberg,et al. High L/D Mars aerocapture for 2001, 2003 and 2005 mission opportunities , 1998 .
[35] L. Bryant,et al. Analytic drag control for precision landing and aerocapture , 1998 .
[36] Brent R. Cobleigh. Development of the X-33 Aerodynamic Uncertainty Model , 1998 .
[37] W. C. Martin,et al. Atomic Spectra Database , 1999 .
[38] Michael E. Tauber,et al. AEROTHERMODYNAMICS OF THE STARDUST SAMPLE RETURN CAPSULE , 1998 .
[39] C. G. Justus,et al. Mars Global Reference Atmospheric Model 2000 Version (Mars-GRAM 2000): Users Guide , 2000 .
[40] John Brophy,et al. Ion propulsion system design for the Comet Nucleus Sample Return mission , 2000 .
[41] David H. Lehman,et al. Results from the Deep Space 1 technology validation mission , 2000 .
[42] Etienne Perot,et al. An analytic aerocapture guidance algorithm for the Mars Sample Return Orbiter , 2000 .
[43] A. Haghighat,et al. Performance of A 3 MCNP™ for Calculation of 3-D Neutron Flux Distribution in a BWR Core Shroud , 2001 .
[44] Ramadas K. Prabhu. Inviscid Flow Computations of Several Aeroshell Configurations for a '07 Mars Lander , 2001 .
[45] Glenn A. Hrinda. Structures for the 3rd Generation Reusable Concept Vehicle , 2001 .
[46] Richard A. Thompson,et al. X-33 Aerodynamic Computations and Comparisons with Wind-Tunnel Data , 2001 .
[47] C. G. Justus,et al. Mars-GRAM 2000: A Mars atmospheric model for engineering applications , 2002 .
[48] Etienne Perot,et al. Importance of an On-board Estimation of the Density Scale Height for Various Aerocapture Guidance Algorithms , 2002 .
[49] Michael J. Patterson,et al. Mission Advantages of NEXT: NASA's Evolutionary Xenon Thruster , 2002 .
[50] James P. Masciarelli,et al. AEROCAPTURE GUIDANCE ALGORITHM COMPARISON CAMPAIGN , 2002 .
[51] Michael J. Patterson,et al. NEXT: NASA's Evolutionary Xenon Thruster , 2002 .
[52] Troy Goodson,et al. Cassini tour redesign for the Huygens mission , 2002 .
[53] Sanford Gordon,et al. NASA Glenn Coefficients for Calculating Thermodynamic Properties of Individual Species , 2002 .
[54] The Seas of Titan , 2003 .
[55] Brian R. Hollis,et al. Preliminary Aerothermodynamics of Titan Aerocapture Aeroshell , 2003 .
[56] C. G. Justus,et al. Mars Global Reference Atmospheric Model (Mars-GRAM) and Database for Mission Design , 2003 .
[57] Swales Aerospace,et al. PLANETARY PROBE MASS ESTIMATION TOOL DEVELOPMENT AND ITS APPLICATION TO TITAN AEROCAPTURE , 2003 .
[58] Robert Bailey,et al. Titan aerocapture mission and spacecraft design overview , 2003 .
[59] Aleta Duvall,et al. Engineering-Level Model Atmospheres for Titan and Neptune , 2003 .
[60] M. Noca. Next generation ion engines: mission performances , 2003 .
[61] Glenn A. Hrinda,et al. STRUCTURAL DESIGN OF THE TITAN AEROCAPTURE MISSION , 2003 .
[62] Mary Kae Lockwood,et al. Titan Aerocapture Systems Analysis , 2003 .
[63] Engineering-level model atmospheres for Titan and Mars , 2003 .
[64] Michelle M. Munk,et al. Aerocapture Technology Development Within the NASA In-Space Propulsion Program , 2003 .
[65] Dinesh K. Prabhu,et al. An Analysis of the Radiative Heating Environment for Aerocapture at Titan , 2003 .
[66] Robert Haw,et al. Approach navigation for a Titan aerocapture orbiter , 2003 .
[67] Peter A. Gnoffo,et al. Computational Aerothermodynamics in Aeroassist Applications , 2001 .
[68] Robert W. Bailey,et al. Titan Explorer mission trades from the perspective of aerocapture , 2003 .
[69] Bernard Laub. Thermal Protection Concepts and Issues for Aerocapture at Titan , 2003 .
[70] Robert J. Haw. Aerocapture navigation at Neptune , 2003 .
[71] James P. Masciarelli,et al. Guidance Algorithms for Aerocapture at Titan , 2003 .
[72] Richard W. Powell,et al. Aerocapture Simulation and Performance for the Titan Explorer Mission , 2003 .
[73] Karl T. Edquist,et al. Configuration, Aerodynamics, and Stability Analysis for a Neptune Aerocapture Orbiter , 2004 .
[74] James P. Masciarelli,et al. Aerocapture Guidance Performance for the Neptune Orbiter , 2004 .
[75] Robert W. Bailey,et al. Mission Trades for Aerocapture at Neptune , 2004 .
[76] Bernard Laub,et al. TPS Challenges for Neptune Aerocapture , 2004 .
[77] C. G. Justus,et al. Mars-GRAM validation with Mars global surveyor data , 2004 .
[78] James Masciarelli,et al. Aerocapture Performance Analysis for a Neptune-Triton Exploration Mission , 2004 .
[79] Chul Park,et al. Stagnation-Point Radiation for Apollo 4 , 2004 .
[80] Dinesh K. Prabhu,et al. Preliminary Convective-Radiative Heating Environments for a Neptune Aerocapture Mission , 2004 .
[81] Glenn A. Hrinda,et al. Structural Design for a Neptune Aerocapture Mission , 2004 .
[82] C. G. Justus,et al. Atmospheric Models for Aerocapture Systems Studies , 2004 .
[83] Mary Kae Lockwood,et al. Neptune Aerocapture Systems Analysis , 2004 .
[84] Deepak Bose,et al. Impact of Flowfield-Radiation Coupling on Aeroheating for Titan Aerocapture , 2005 .
[85] Robert W. Bailey,et al. Cost-Benefit Analysis of the Aerocapture Mission Set , 2005 .
[86] C. G. Justus,et al. Global MGS TES data and Mars-GRAM validation , 2005 .
[87] Richard W. Powell,et al. Entry Configurations and Performance Comparisons for the Mars Smart Lander , 2006 .
[88] Karl T. Edquist,et al. Aeroheating Environments for a Mars Smart Lander , 2002 .
[89] The application of general circulation models to the atmospheres of terrestrial-type moons of the giant planets , 2013 .