NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The Gold Rush: A simulated commercial air transportation studyThe remotely piloted vehicle (RPV) GoldRush was designed to complete the mission of transporting passengers in AeroWorld at a lower cost per seat per thousand feet (CPSPK) than the competition, the HB-40. There were two major factors which were constant considerations in the design process. The cost of manufacturing was the most important. In light of this, the designs were kept as simple as possible while considering trade-offs in performance. For example, the wing was not tapered so that several ribs could be cut at one time. Also of major importance was the takeoff distance. In order to serve all the cities in AeroWorld it was necessary to maintain a takeoff distance requirement of 24 feet. The takeoff distance proved to be the number one force in driving the design process. The Astro 25 engine and 13 inch propellor, a large wing area, and the high lift Wortmann airfoil were all chosen in order to satisfy this objective.
Document ID
19940020520
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clarke, Amanda
(Notre Dame Univ. IN, United States)
Degiorgio, Chris
(Notre Dame Univ. IN, United States)
Galka, Edmund
(Notre Dame Univ. IN, United States)
Stumm, Albert
(Notre Dame Univ. IN, United States)
Valenta, Lisa
(Notre Dame Univ. IN, United States)
Winter, Tom
(Notre Dame Univ. IN, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1993
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-195528
NAS 1.26:195528
Report Number: NASA-CR-195528
Report Number: NAS 1.26:195528
Accession Number
94N25002
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available