2026-03-15T05:42:02Z https://jaxa.repo.nii.ac.jp/oai

oai:jaxa.repo.nii.ac.jp:00006356 2023-06-21T07:57:15Z 1887:1891 9:789:1031:1066

Spacecraft charging phenomena and spacecraft design guidelines Frederickson, Arthur Robb 宇宙機帯電 航空宇宙環境 宇宙機設計 表面帯電 電場 電子放射 静電放電 地上試験 電磁遮蔽 spacecraft charging aerospace environment spacecraft design surface charging electric field electron radiation electrostatic discharge ground test electromagnetic shielding (1) ONE PHENOMENON, But Two Primary Manifestations: 1. Surface Charging. 2. Internal Oharging. (2) Existing Design Guidelines for Spacecraft Charging: 1. Guidelines are far from complete at this time, yet there are many. (3) Wide Assortment of Phenomena in Differing Applications: 1. CASE STUDY 1: In-space Insulator Pulsing. 2. CASE STUDY 2: Coupling from a Breakdown into a Circuit. (4) Spacecraft Failure Studies: 1. ELECTRIC FIELD FROM CHARGE IN INSULATING MATERIAL IS A PRIMARY CAUSE OF SPACECRAFT ON-ORBIT ANOMALIES. (5) Electric Field Controls the ESD Pulse Rate and Pulse Amplitude. (6) Complete solution of the problem requires knowledge of electric field -very difficult; Ongoing Studies. 資料番号: AA0049206041 レポート番号: JAXA-SP-05-001E conference paper 宇宙航空研究開発機構 Japan Aerospace Exploration Agency (JAXA) 2005-08-01 application/pdf 宇宙航空研究開発機構特別資料 JAXA-SP-05-001E 312 330 JAXA Special Publication: 9th Spacecraft Charging Technology Conference 1349-113X AA11984031 https://jaxa.repo.nii.ac.jp/record/6356/files/49206041.pdf https://jaxa.repo.nii.ac.jp/records/6356 eng