Inflatable re-entry technologies: Flight demonstration and future prospects

Citation
L. Marraffa et al., Inflatable re-entry technologies: Flight demonstration and future prospects, ESA B, (103), 2000, pp. 78-85
Categorie Soggetti
Aereospace Engineering
Journal title
ESA BULLETIN-EUROPEAN SPACE AGENCY
ISSN journal
03764265 → ACNP
Issue
103
Year of publication
2000
Pages
78 - 85
Database
ISI
SICI code
0376-4265(200008):103<78:IRTFDA>2.0.ZU;2-R
Abstract
In cooperation with Astrium-I (formerly DASA), NPO Lavochkin and the Europe an Commission, ESA has developed and launched a capsule that re-entered the Earth's atmosphere protected by an inflatable heat shield. During the same mission, the newly developed Russian Fregat upper stage was also returned to Earth using the same technology. The last phase of the descent in both c ases was performed with no parachute, allowing substantial savings in launc h volume and mass. Obvious future applications for this new re-entry techno logy include International Space Station sample return, the delivery of net works of small stations to the Martian surface, and the return to Earth of launcher upper stages.