In an example, a recovery system is shown, the recovery system comprising: a housing; a parasail comprising a canopy coupled within the housing fastened by a releasable fastener, wherein the parasail is compressed into a compact mass and is configured to rapidly expand; primary ballistics attached to the parasail, wherein the primary ballistics are configured to launch the parachute from the housing; and a guidance system within the housing wherein the guidance system is configured to steer the parasail and guide the recovery system to a landing site.
BALLISTICALLY-DEPLOYED CONTROLLABLE PARASAIL
BALLISTISCH ENTFALTETER STEUERBARER GLEITSCHIRM
PARAVOILE COMMANDABLE À DÉPLOIEMENT BALISTIQUE
2021-11-24
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Optimal ballistically captured Earth–Moon transfers
Elsevier | 2012
|Optimal ballistically captured Earth–Moon transfers
Online Contents | 2012
|