درباره ما
NASA-HDBK-7005
DYNAMIC ENVIRONMENTAL CRITERIA
Year: 2001
Abstract: Purpose. The purpose of this handbook is to summarize and assess the following:
a. The dynamic environments that a spacecraft might be exposed to during its service life from the completion of its manufacture to the completion of its mission.
b. The state-of-the-art procedures for predicting the dynamic excitations (loads) produced by the dynamic environments.
c. The state-of-the-art procedures for predicting the structural responses to the dynamic excitations.
d. The state of the art procedures for establishing dynamic criteria with appropriate margins for the design and testing of a spacecraft and its components.
e. The equipment and procedures used to test a spacecraft and its components.
a. The dynamic environments that a spacecraft might be exposed to during its service life from the completion of its manufacture to the completion of its mission.
b. The state-of-the-art procedures for predicting the dynamic excitations (loads) produced by the dynamic environments.
c. The state-of-the-art procedures for predicting the structural responses to the dynamic excitations.
d. The state of the art procedures for establishing dynamic criteria with appropriate margins for the design and testing of a spacecraft and its components.
e. The equipment and procedures used to test a spacecraft and its components.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:12:02Z | |
| date available | 2017-09-04T16:12:02Z | |
| date copyright | 03/13/2001 | |
| date issued | 2001 | |
| identifier other | SNTRFBAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/75271 | |
| description abstract | Purpose. The purpose of this handbook is to summarize and assess the following: a. The dynamic environments that a spacecraft might be exposed to during its service life from the completion of its manufacture to the completion of its mission. b. The state-of-the-art procedures for predicting the dynamic excitations (loads) produced by the dynamic environments. c. The state-of-the-art procedures for predicting the structural responses to the dynamic excitations. d. The state of the art procedures for establishing dynamic criteria with appropriate margins for the design and testing of a spacecraft and its components. e. The equipment and procedures used to test a spacecraft and its components. | |
| language | English | |
| title | NASA-HDBK-7005 | num |
| title | DYNAMIC ENVIRONMENTAL CRITERIA | en |
| type | standard | |
| page | 249 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2001 | |
| contenttype | fulltext |