Author: American Institute of Aeronautics and Astronautics
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 288
Book Description
AIAA Entry Technology Conference, Williamsburg & Hampton, Va., October 12-14, 1964
Author: American Institute of Aeronautics and Astronautics
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 288
Book Description
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 288
Book Description
Astronautics and Aeronautics, 1964
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 552
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 552
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1176
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1176
Book Description
Summary of the Eleventh Meeting of the Refractory Composites Working Group
Author: Darrell R. James
Publisher:
ISBN:
Category : Refractory materials
Languages : en
Pages : 1496
Book Description
Publisher:
ISBN:
Category : Refractory materials
Languages : en
Pages : 1496
Book Description
Technical Papers
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 286
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 286
Book Description
Space Simulation
Author: Joseph C. Richmond
Publisher:
ISBN:
Category : Space environment
Languages : en
Pages : 988
Book Description
Publisher:
ISBN:
Category : Space environment
Languages : en
Pages : 988
Book Description
Planetary Atmospheres
Author:
Publisher:
ISBN:
Category : Planets
Languages : en
Pages : 452
Book Description
Publisher:
ISBN:
Category : Planets
Languages : en
Pages : 452
Book Description
AIAA Bulletin
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2244
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2244
Book Description
Apollo Ablator Thermal Performance at Superorbital Entry Velocities
Author: Donald M. Curry
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 36
Book Description
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.
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 36
Book Description
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
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 636
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 636
Book Description