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Solid State Inflation Balloon Active Deorbiter: Scalable Low-Cost Deorbit System for Small SatellitesThe 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.
Document ID
20160007907
Acquisition Source
Ames Research Center
Document Type
Other - Brief Communication/Note
Authors
Huang, Adam
(Arkansas Univ. System Fayetteville, AR, United States)
Date Acquired
June 27, 2016
Publication Date
April 20, 2016
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
FS-2016-04-07-ARC
ARC-E-DAA-TN31591
Funding Number(s)
CONTRACT_GRANT: NNX15AW38A
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Drag balloon
Small satellites
Active deorbiting system
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