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Aerospace vehicle design, spacecraft section. Volume 1The objective was to create a manned Martian aircraft which can perform: scientific surveys of particular sites distant from the base; a deployment of scientific instrument packages by air drop that land rovers cannot accomplish; and rescue operations. Designing the airfoil requires a wing which can operate within the low Reynolds numbers apparent on Mars. The airfoil, NASA NLF(1)-1015 was chosen. The design of the aircraft is comparable to a P-38 military aircraft. The aircraft uses fuel cells to power the two propellers. A rocket-assisted takeoff is necessary to enable Romulus to liftoff. Although the design and creation of Romulus would be an expensive adventure, such a vehicle could be most useful in evaluating the Mars surface and in creating a habitat for mankind.
Document ID
19890010750
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-184741
AAE-241-VOL-1
NAS 1.26:184741
Report Number: NASA-CR-184741
Report Number: AAE-241-VOL-1
Report Number: NAS 1.26:184741
Accession Number
89N20121
Funding Number(s)
CONTRACT_GRANT: NGT-21-002-080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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