Abstract
The present paper presents work on developing and flight testing a Mars prototype aircraft using inflatable-rigidizable wings under the NASA Workforce Development program. Undergraduate student teams have developed a test vehicle to determine the feasibility of using inflatable-rigidizable wings in extra-terrestrial missions. The wings are constructed of an outer composite layer impregnated with a UV curable resin and an inner inflatable bladder. The wings are stowed in the fuselage, deploy when inflated, and rigidize with exposure to UV radiation; pressurization is not required after rigidization. Vehicle, wing and avionics designs are discussed and results from low and high altitude test flights are presented. The project culminated in a successful high altitude flight test with deployment and rigidization of the wing under Mars like conditions.
Original language | English |
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Pages | 3189-3200 |
Number of pages | 12 |
DOIs | |
State | Published - 2005 |
Event | 43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States Duration: Jan 10 2005 → Jan 13 2005 |
Conference
Conference | 43rd AIAA Aerospace Sciences Meeting and Exhibit |
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Country/Territory | United States |
City | Reno, NV |
Period | 1/10/05 → 1/13/05 |
ASJC Scopus subject areas
- General Engineering