DocumentCode
2068027
Title
A historical review of Inflatable Aerodynamic Decelerator technology development
Author
Smith, Brandon P. ; Tanner, Christopher L. ; Mahzari, Milad ; Clark, Ian G. ; Braun, Robert D. ; Cheatwood, F. McNeil
Author_Institution
Daniel Guggenheim Sch. of Aerosp. Eng., Georgia Inst. of Technol., Atlanta, GA, USA
fYear
2010
fDate
6-13 March 2010
Firstpage
1
Lastpage
18
Abstract
Viking-era deployable decelerator technology has been employed for several planetary probe missions at Earth and within other planetary atmospheres. Numerous system studies in the past fifty years demonstrate the benefit of developing a new decelerator technology capable of operating at higher Mach numbers and higher dynamic pressures than existing decelerators allow. The deployable Inflatable Aerodynamic Decelerator (IAD) is one such technology. This survey paper describes the development history of the IAD from its conception in the 1960´s to the present day. Major findings in primary IAD sub-disciplines for the foremost configurations are discussed. Quantitative engineering data from prior testing is reproduced directly, while qualitative conclusions are referenced in the literature. This work provides a summary of past and present IAD technology development efforts and shows data in a manner useful for today´s mission designers.
Keywords
Mach number; aerodynamics; aerospace components; computational fluid dynamics; drag; history; hypersonic flow; space research; supersonic flow; Earth; Mach numbers; drag; dynamic pressures; dynamic testing; hypersonic IAD; inflatable aerodynamic decelerator technology development; planetary atmospheres; planetary probe missions; supersonic IAD; viking era deployable decelerator technology; Aerodynamics; History; NASA; Probes; Shape; Space technology; Stability; Testing; Vehicle dynamics; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2010 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-3887-7
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2010.5447013
Filename
5447013
Link To Document