The electrical architecture of a parafoil technology demonstrator

14th Aerodynamic Decelerator Systems Technology Conference

Volumn , Issue , 1997, Pages 150-157

  Hollestelle, Pieter M N ^a  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; LANDING;

DEVELOPMENT APPROACH; ELECTRICAL ARCHITECTURE; EUROPEAN SPACE AGENCY; FLIGHT TEST PROGRAMS; MECHANICAL LAYOUT; NATIONAL AEROSPACE LABORATORIES; ONBOARD COMPUTER SYSTEM; PARAFOIL SYSTEMS;

SOFTWARE TESTING;

EID: 84976513379     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1997-1467     Document Type: Conference Paper

References (4)

1. Hummeltenberg, Behr, Starke. PTD Key System Requirements Doc-No.: HT-TN-E9.7-106 DASA
2. P.M.N. Hollestelle, Electrical Architecture and Subsystem definition for PTTV, part 1 Doc- No.: HT -TN -E9.7-007-FSS
3. P.H. van Rossum, Electrical Architecture and Subsystem definition for PTTV, part 3 Doc- No.: HT -TN -E9.7-007-FSS
4. Behr., PTD test objectives Doc- No.: HT-TN-E9.7-012-DASA