Applying MEMS technology to field, flight & space deployable systems

ICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities

Volumn , Issue , 2001, Pages 246-255

  Shams, Q A ^a   Moniuszko, M ^a   Ingham, J C ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC MEASURING INSTRUMENTS; METEOROLOGICAL INSTRUMENTS; SPACE APPLICATIONS; SPACE FLIGHT; SPACECRAFT PROPULSION; WIND TUNNELS;

SPACE DEPLOYABLE SYSTEMS;

MICROELECTROMECHANICAL DEVICES;

EID: 0035167123     PISSN: 07302010     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Micro - And nanotechnology for space systems
2. Comparison of 6H-SiC, 3C-SiC, and Si for power devices
3. Vertical tail buffeting alleviation using piezoelectric actuators (ACROBAT) program
4. Progress and new technologies in buffet alleviation
5. Vortex control for the attenuation of F in buffet
6. Tangential leading-edge blowing on a combat aircraft configuration
7. Investigation of buffet load alleviation on a scaled F-15 twin tail model
8. Wind-tunnel investigation of aerodynamic and tail buffet characteristics of leading-edge extension modifications to the F/A-18
9. Full-scale wind-tunnel pressure measurements on an F/A-18 tail during buffet
10. Full-scale wind-tunnel studies of F/A-18 tail buffet
11. Reduction of vertical tail buffett response using active control