Compliance with the United Nations recommended 25-year maximum orbital lifetime requirement will restrict future standard CubeSat nanosatellite deployments to altitudes below 600 km. This paper describes a deployable aerodynamic drag device that can be incorporated in basic CubeSat satellite units that can meet the 25-year orbital lifetime constraint for initial orbit perigees of up to 900 km.
A de-orbit system design for CubeSat payloads
01.06.2011
1306300 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A COMPACT LAUNCH LOCK SYSTEM FOR CUBESAT-SIZED PAYLOADS
TIBKAT | 2020
|Development of intelligent remote sensing payloads for CubeSat applications
SPIE | 2025
|