A Methodology for Using Optimal MSIS Parameters Retrieved From SSULI Data to Compute Satellite Drag on LEO Objects (AAS 99-382)
A Methodology for Using Optimal MSIS Parameters Retrieved From SSULI Data to Compute Satellite Drag on LEO Objects (AAS 99-382)
- New search for: Nicholas, A. C.
- New search for: Picone, J. M.
- New search for: Thonnard, S. E.
- New search for: American Astronautical Society
- New search for: American Institute of Aeronautics and Astronautics
- New search for: Nicholas, A. C.
- New search for: Picone, J. M.
- New search for: Thonnard, S. E.
- New search for: Howell, K. C.
- New search for: American Astronautical Society
- New search for: American Institute of Aeronautics and Astronautics
Document information
A Methodology for Using Optimal MSIS Parameters Retrieved From SSULI Data to Compute Satellite Drag on LEO Objects (AAS 99-382)
Conference, Astrodynamics 1999; Advances in the astronautical sciences ; 1999 ; Girdwood, AK
2000-01-01
16 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Similar titles
An evaluation of Jacchia and MSIS 90 atmospheric models with CBERS data
| British Library Conference Proceedings | 2001
An evaluation of Jacchia and MSIS 90 atmospheric models with CBERS data
| Online Contents | 2001
Faster side impact development using MIRA's side impact simulation ( MSIS ) technique
| Automotive engineering | 1996
Faster side impact development using MIRA's side impact simulation (MSIS) technique
| British Library Conference Proceedings | 1996
Implementing the MSIS Atmospheric Density Model in OCEAN (AAS 03-166)
| British Library Conference Proceedings | 2003