Power system comparisons for a High Altitude Long Endurance (HALE) Remotely Operated Aircraft (ROA)

Collection of Technical Papers - AIAA 5th ATIO and the AIAA 16th Lighter-than-Air Systems Technology Conference and Balloon Systems Conference

Volumn 2, Issue , 2005, Pages 933-945

  Atreya, Shailesh ^a,c   Mata, Marianne ^a,c   Jones, Russ ^a,d   Kohout, Lisa ^b,e  

^a BOEING COMPANY   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c MC H013 C320   (United States)

^d Avionics Design and Analysis   (United States)

^e Electrochemistry Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

HIGH ALTITUDE LONG ENDURANCE (HALE); REMOTELY OPERATED AIRCRAFT (ROA);

AIRCRAFT; ELECTRIC POWER SYSTEMS; INTERNAL COMBUSTION ENGINES; RESEARCH; SOLID OXIDE FUEL CELLS;

REMOTELY OPERATED VEHICLES;

EID: 33644500439     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Atreya, Jones, Mata, Stoia, "Solid Oxide Fuel Cell Technology for HALE Operating Environments (SOFTSHOE); Revolutionary Aero Space Engine Research (RASER) Program", NAS3-01140 Task Order 24, 2005
2. Perkins and Hage, "Airplane Performance Stability and Control", John Wiley and Sons. Inc., Copyright 1949
3. th Edition, EG&G Services, Parsons Inc., Science Applications International Corporation. US Department of energy contract no, DE-AM26-99FT40575. October 2002
4. Mankins, John C., "Technology Readiness Levels: A White Paper", April 6, 1995.