Flexible wing deployment device Patent
Deployment system for flexible wing with rigid superstructure
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Deployment system for flexible wing with rigid superstructure
Preventing pressure buildup in electrochemical cells by reacting palladium oxide with evolved hydrogen
Cryogenic storage system for gases onboard spacecraft
Using ethylene oxide in preparation of sterilized solid rocket propellants and encapsulating materials
Accel and focus electrode design for ion engine with improved efficiency
Water cooled solenoid capable of producing magnetic field intensities up to 100 kilogauss
Closed loop radio communication ranging system to determine distance between moving airborne vehicle and fixed ground station
Multiple wavelength radiation measuring instrument for determining hot body or gas temperature
Liquid propellant tank design with semitoroidal bulkhead
Proportional controller for regulating aircraft or spacecraft motion about three axes
Electro-optical/computer system for aligning large structural members and maintaining correct position
Piezoelectric transducer for detecting and measuring micrometeoroids
Electrical connection for printed circuits on common board, using bellows principle in rivet
Phase shift data transmission system with pseudo-noise synchronization code modulated with digital data into single channel for spacecraft communication
Variable time constant, wide frequency range smoothing network for noise removal from pulse chains
Flexible rocket motor nozzle closure device to aid ignition and protect rocket chamber from foreign objects
Automatic baseline stabilization for ionization detector used in gas chromatograph
Regenerative cooling system for small rocket engine having restart capability and using noncryogenic hypergolic propellants