NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High-altitude reconnaissance aircraftAt the equator the ozone layer ranges from 65,000 to 130,000+ ft, which is beyond the capabilities of the ER-2, NASA's current high-altitude reconnaissance aircraft. This project is geared to designing an aircraft that can study the ozone layer. The aircraft must be able to satisfy four mission profiles. The first is a polar mission that ranges from Chile to the South Pole and back to Chile, a total range of 6000 n.m. at 100,000 ft with a 2500-lb payload. The second mission is also a polar mission with a decreased altitude and an increased payload. For the third mission, the aircraft will take off at NASA Ames, cruise at 100,000 ft, and land in Chile. The final mission requires the aircraft to make an excursion to 120,000 ft. All four missions require that a subsonic Mach number be maintained because of constraints imposed by the air sampling equipment. Three aircraft configurations were determined to be the most suitable for meeting the requirements. The performance of each is analyzed to investigate the feasibility of the mission requirements.
Document ID
19930020524
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yazdi, Renee Anna
(California State Polytechnic Univ. Pomona, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: Universities Space Research Association, Houston, Proceedings of the Seventh Annual Summer Conference. NASA(USRA: University Advanced Design Program
Subject Category
Aircraft Design, Testing And Performance
Accession Number
93N29713
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available