| タイトル | Solid State Inflation Balloon Active Deorbiter: Scalable Low-Cost Deorbit System for Small Satellites |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160007907 |
| 著者（英） | Huang, Adam |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2016-04-20 |
| 言語 | eng |
| 内容記述 | The goal of the Solid State Inflation Balloon Active Deorbiter project is to develop and demonstrate a scalable, simple, reliable, and low-cost active deorbiting system capable of controlling the downrange point of impact for the full-range of small satellites from 1 kg to 180 kg. The key enabling technology being developed is the Solid State Gas Generator (SSGG) chip, generating pure nitrogen gas from sodium azide (NaN3) micro-crystals. Coupled with a metalized nonelastic drag balloon, the complete Solid State Inflation Balloon (SSIB) system is capable of repeated inflation/deflation cycles. The SSGG minimizes size, weight, electrical power, and cost when compared to the current state of the art. |
| NASA分類 | Electronics and Electrical Engineering |
| レポートNO | ARC-E-DAA-TN31591
FS-2016-04-07-ARC |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
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