Mars Express power subsystem in-flight experience

SpaceOps 2006 Conference

Volumn , Issue , 2006, Pages

  Ferretti, R ^a   Denis, M ^b   Moorhouse, A ^b   Dudley, G ^c   Ecale, E ^d   Rabenau, E ^e   Page, O ^f   Schulster, J ^g   Ormston, T ^b  

^a VEGA   (Germany)

^b ESA ESOC   (Germany)

^c EUROPEAN SPACE AGENCY   (Netherlands)

^d AIRBUS GROUP INNOVATIONS   (Germany)

^e NOVA Space Associates Ltd   (United Kingdom)

^f Telecommunication business unit   (United Kingdom)

^g SciSys Ltd   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMMUNICATION METHOD; DEPTH OF DISCHARGES; EXTREME DISCHARGES; MISSION MANAGEMENT; SCIENCE COMMUNITY; SCIENCE OPERATIONS; SPACECRAFT MANUFACTURERS; TECHNICAL EXPERTS;

HUMAN RESOURCE MANAGEMENT; SPACE FLIGHT;

SPACECRAFT;

EID: 84884422306     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. th European Space Power Conference, Stresa Italy, May 2005.
2. C. Thwaite. Private communication
3. Mission Planning Experience Gained from the Mars Express Mission. E. Rabenau and All, Paper Number: AIAA-2006-5800.
4. Long Term Preservation of Mars Express. Z. Mounzer, R Ferretti and All, Paper Number: AIAA-2006-5699.
5. MARS EXPRESS Power System Optimum Power Extraction Method, MEX-TER-RP-0016, 21-11-03
6. ROSETTA Power Conditioning Unit Design Description, RO-TER-DD-3001, 05-07-01
7. MISSION AND SPACECRAFT DESCRIPTION, MEX-MMT-MA-1091 15-03-03