Full-scale dynamic landing-impact investigation of a prototype lunar module landing gear
Full scale dynamic landing impact investigation of prototype lunar module landing gear
SEARCH · Engineering Papers
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.
Full scale dynamic landing impact investigation of prototype lunar module landing gear
Rocket-borne mass spectrometer-getter system for D region studies - flight prototype
Construction of cold cathode quadrupole mass spectrometer as flight prototype
Prototype microfilm storage and display unit with 6000 frame capacity on 16 mm film, 12 lb weight, and designed for spacecraft use
Performance tests of prototype liquid ammonia spacecraft attitude control systems
Electrostatic zero-gravity work bench prototype for spacecraft use
Lightweight magnetic material for armature of magnetic circuit for prototype restraint footwear for astronaut IVA
Underwater tests of prototype construction of selected mobility and restraint device
Multichip hybrid fabrication techniques for prototype function generator circuits
Characteristics of prototype waste collection system for spacecraft applications
Design of prototype systems performance evaluation console as man machine interface
Laboratory prototype system for acquisition, automatic analysis, and display of astronaut electroencephalographic and electro-oculographic signals, and spacecraft noise effects on sleep
Space shuttle structural prototype design, fabrication and test program
Prototype lunar gravity simulator for studies of reduced gravity effects on human self locomotive capability, using magnetic air bearings and body support system
Prototype cloud physics laser nephelometer design and performance, determining droplet concentration and size from scattered light pulse count and amplitudes
Prototype electrolyzer for generating oxygen from water vapor under various atmospheric conditions, noting spacecraft cabin application
Space compatible flight prototype ion engine power conditioning system design for Hg thrustor using oxide cathode
Flight prototype electrostatic ballistic pendulum momentum transducer