Effect of Power System Technology and Mission Requirements on High Altitude Long Endurance Aircraft
- Author(s):
- Colozza, Anthony J. ( Sverdrup Technology, Inc. )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1994
- Issue:
- NASA-CR-194455
- No.:
- G3/07 020753
- Pt.:
- NAS 1.26:194455
- Paper no.:
- N94-25200
- Page(from):
- 1
- Page(to):
- 22
- Pages:
- 22
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
|
1
Technical Paper
Effect of Date and Location on Maximum Achievable Altitude for a Solar Powered Aircraft
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
|
National Aeronautics and Space Adminstration |
8
Technical Paper
Power System Comparisons for a High Altitude Long Endurance (HALE) Remotely Operated Aircraft (ROA)
American Institute of Aeronautics and Astronautics |
|
Society of Automotive Engineering, Inc. |
9
Technical Paper
System Analysis Applied to Autonomy: Application to High-Altitude Long-Endurance Remotely Operated Aircraft
American Institute of Aeronautics and Astronautics |
|
National Aeronautics and Space Adminstration |
10
Technical Paper
Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft
American Institute of Aeronautics and Astronautics |
|
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
|
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |