Spin Stability of Sounding Rocket Secondary Payloads Following High Velocity Ejections
The Auroral Spatial Structures Probe (ASSP) mission is a sounding rocket mission studying solar energy input to space weather. ASSP requires the high velocity ejection (up to 50 m/s) of 6 secondary payloads, spin stabilized perpendicular to the ejection velocity. The proposed scientific instrumentat...
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| Format: | Others |
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DigitalCommons@USU
2013
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| Online Access: | https://digitalcommons.usu.edu/etd/1961 https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=2967&context=etd |