The Orion space vehicle is designed to requirements for both direct attachment and indirect effects of lightning. Both sets of requirements are based on a full threat 200kA strike, in accordance with constraints and guidelines contained in SAE ARP documents applicable to both commercial and military aircraft and space vehicles. This paper describes the requirements as levied against the vehicle, as well as the means whereby the design shows full compliance.
Lightning Protection for the Orion Space Vehicle
2015
10 pages
Report
No indication
English
Lightning Protection for the Orion Space Vehicle
AIAA | 2015
|Lightning Protection for the Orion Space Vehicle
NTRS | 2015
|Lightning Protection for the Orion Space Vehicle
NTRS | 2015
|Lightning Protection for the Orion Space Vehicle (AIAA 2015-3320)
British Library Conference Proceedings | 2015
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