Many in the space weather community consider our understanding of the buoyancy of the thermosphere and its effects on the orbits of satellites in Low Earth Orbit (LEO) to be insufficient during short time frames. Disclosed herein is an approach for making on-demand thermosphere buoyancy measurements using a deployable low mass retroreflector with CubeSat-like dimensions. A CubeSat storing many retroreflectors can dispense one or more of these passive satellites according to a predetermined schedule or on-command, in response to an observed space weather phenomenon like a coronal mass ejection. With measurements of the orbit decay from these passive satellites, a better understanding of the relationship between space weather and orbital decay can be established with relatively low cost.
Retroreflector with load-biased hinges
Issue
Date
Publication Date
Patent No.
11,119,256
Category
Device or Machine (e.g. such as sensors or engine or circuits)
Keywords: hinge, v-spring, hive
International Class: G02B 5/13 (20060101), G01B 11/25 (20060101)