A Parametric Study on the Liquid Droplet Radiator for the Space Solar Power Satellite

Details A Parametric Study on the Liquid Droplet Radiator for the Space Solar Power Satellite A Parametric Study on the Liquid Droplet Radiator for the Space Solar Power Satellite

Jan 2002

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002iaf..confe.765t&link_type=abstract

IAF abstracts, 34th COSPAR Scientific Assembly, The Second World Space Congress, held 10-19 October, 2002 in Houston, TX, USA.,

Physics

Scientific paper

satellites (SPS). The liquid droplet radiator (LDR) is a strong candidate for resolving that issue. The lightweight structure, strong resistance to meteorite impacts, a small storage volume at launch and an easy deployment in space make it a very attractive heat rejection system for SPS. on the ground with (a) 10 MW, (b) 100 MW and (c) 1.0 GW electricity using parameters that a LDR functions properly under. The parameters were acquired through ground experiments including the microgravity environment. case of (a) while it is not still easy to realize the LDR in case of (b) and (c) from a viewpoint of .the number of necessary launches for the construction. Advanced technologies of transferring lager mass in orbit at lower cost are needed for realizing the LDR of (b) and (c).

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