SMALL RECOVERABLE PAYLOAD FOR DEPLOYABLE SOUNDING ROCKET EXPERIMENTS

被引:0
|
作者
Sundberg, T. [1 ]
Ivchenko, N. [1 ]
Borglund, D. [2 ]
Ahlen, P. [1 ]
Gustafsson, M. [1 ]
Jonsson, C. [1 ]
Juhlen, J. [1 ]
Neuner, O. [1 ]
Sandstrom, J. [1 ]
Sund, E. [1 ]
Wartelski, M. [1 ]
Westlund, C. [1 ]
Xin, L. [1 ]
机构
[1] Royal Inst Technol KTH, Space & Plasma Phys, Stockholm, Sweden
[2] Royal Inst Technol KTH, Dept Aeronaut & Vehicle Engn, Stockholm, Sweden
关键词
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中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
We present a design of a small payload for deployment from sounding rockets. The payload is intended for measurements in the ionosphere and the acquired data is stored onboard. For a secure recovery of the data and possible re-use of the payload, an inflatable structure is deployed during the payload descent. This reduces the payload speed and protects it from ground impact. On the ground, a localization system is activated, sending the payload position via a satellite link, and providing a radio beacon signal. The proposed small payload will allow high time resolution multipoint measurements in the ionosphere with small separation distances, thus allowing to address a number of unresolved questions in the field.
引用
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页码:281 / 284
页数:4
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