A PC-based design and analysis system for lighter-than-air unmanned vehicles

2nd AIAA "Unmanned Unlimited" Conference and Workshop and Exhibit

Volumn , Issue , 2003, Pages

  Ozoroski, Thomas A ^a   Mas, Kyle G ^a   Hahn, Andrew S ^b  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRSHIPS;

DESIGN AND ANALYSIS; DESIGN TECHNIQUE; DIRECT CALCULATION; MICROSOFT EXCEL; MISSION REQUIREMENTS; SOLAR ARRAY AREA; STATION-KEEPING; WIND SPEED PROFILES;

DESIGN;

EID: 84896030071     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Khoury, Gabriel A.; Gillett, J. David: Airship Technology. Cambridge University Press, 1999.
2. ILC Dover: "Design Definition of a Lighter Than Air (LTA) High Altitude Powered Platform (HAPP)", NASA CR-168350-Vol-2, November 1982.
3. Power Computing Solutions, Inc.: "Electric Power System for High Altitude UAV Technology Survey", NAS2-96011, November 1997.
4. NOAA, NASA, USAF.: U.S. Standard Atmosphere,1976. U.S. Government Printing Office, 1976.
5. «Goodyear Blimp Technical Statistics». www.goodyearblimp.com.
6. Lockheed Missiles and Space Co.: "HI-SPOT Conceptual Design Study Final Report", N62269-81-C-0276, March 1982.
7. Petrone, Francis J.; Wessel, Paul R.: "HASPA Design and Flight Test Objectives", AIAA 75-924, July 1975.
8. Strganac, Thomas W.: "Wind Study for High Altitude Platform Design". NASA Reference Publication 1044.