AIAA Entry Technology Conference, Williamsburg & Hampton, Va., October 12-14, 1964

AIAA Entry Technology Conference, Williamsburg & Hampton, Va., October 12-14, 1964 PDF Author: American Institute of Aeronautics and Astronautics
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ISBN:
Category : Astrodynamics
Languages : en
Pages : 288

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AIAA Entry Technology Conference, Williamsburg & Hampton, Va., October 12-14, 1964

AIAA Entry Technology Conference, Williamsburg & Hampton, Va., October 12-14, 1964 PDF Author: American Institute of Aeronautics and Astronautics
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 288

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Astronautics and Aeronautics, 1964

Astronautics and Aeronautics, 1964 PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 552

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1176

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Summary of the Eleventh Meeting of the Refractory Composites Working Group

Summary of the Eleventh Meeting of the Refractory Composites Working Group PDF Author: Darrell R. James
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ISBN:
Category : Refractory materials
Languages : en
Pages : 1496

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Technical Papers

Technical Papers PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 286

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Space Simulation

Space Simulation PDF Author: Joseph C. Richmond
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ISBN:
Category : Space environment
Languages : en
Pages : 988

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Planetary Atmospheres

Planetary Atmospheres PDF Author:
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ISBN:
Category : Planets
Languages : en
Pages : 452

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AIAA Bulletin

AIAA Bulletin PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 2244

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Apollo Ablator Thermal Performance at Superorbital Entry Velocities

Apollo Ablator Thermal Performance at Superorbital Entry Velocities PDF Author: Donald M. Curry
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ISBN:
Category : Materials
Languages : en
Pages : 36

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Objectives of the Apollo 4 and 6 missions included the demonstration of the capability of the ablative heat shield to survive entry at lunar-return velocities and the collection of data necessary to support the analytical qualification of the ablative heat shield for manned lunarreturn missions. Results of ground test programs, as well as the Apollo 4 and 6 flight tests, are discussed in relation to the verification of the analytical ablation model, Ablator cores taken from the Apollo command module were evaluated to obtain the thermophysical property values used in the analytical model. Temperatures were measured by thermocouples located in depth in the ablator. Char-thickness measurements were obtained from char sensors in the heat shield and from ablator cores. The results of the thermal performance evaluation and comparisons of measured and predicted data have been used to establish a confidence level in the analytical model used to make preflight predictions and will provide the information necessary to improve prediction techniques.

NASA Technical Report

NASA Technical Report PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 636

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