Two /2/ way, latching, dc solenoid control valve Final report, 1 Mar. - 28 Dec. 1965
Two way, latching, dc solenoid valve to isolate reaction control engine clusters from main hypergolic propellant supply system
CONTROL VALVE↗
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Results for “latches”
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.
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Latch diaphragm release mechanism
Latch diaphragm release mechanism for payload separation in space
PAYLOAD↗
Latching ferrite switch Final report, May 1967 - Jun. 1968
Ferrite latching switch and combiner with 33 circulators having low insertion loss
Source record↗
Latch and trip mechanisms for triggering a large force with a small one.
Latch and trip mechanisms for triggering large loads with small loads through interrupted motion
Tuttle, S. B.↗
Electronic position indicator for latching solenoid valves
Electronic position indicator for latching solenoid valves in SNAP 8 ground test facility
Frye, R. J.↗
A technique for analyzing latching dynamics and loads induced during spacecraft docking
Three dimensional latching dynamics and loads induced during Apollo spacecraft docking, using linear stiffness or flexibility matrices for structural elasticity
Glynn, P. C.↗
Helmet assembly and latch means therefor Patent
Transparent polycarbonate resin, shell helmet and latch design for high altitude and space flight
Jones, R. L.↗
Quick disconnect latch and handle combination Patent
Quick disconnect latch and handle combination for mounting articles on walls or supporting bases in spacecraft under zero gravity conditions
Coker, L. R.↗
Latching mechanism Patent
Design, development, and characteristics of latching mechanism for operation in limited access areas
Holman, E. V.↗
Circuit breaker utilizing magnetic latching relays Patent
Relay circuit breaker with magnetic latching to provide conductive and nonconductive paths for current devices
Reinhold, H. W.↗
Apollo 14 mission: Failure to achieve docking probe capture latch engagement
Six docking attempts were required in order to successfully achieve capture latch engagement during the transposition and docking phase following translunar injection. After docking, the probe and drogue were examined by the crew. Probe operation appeared normal and radial marks were noted on the drogue. During all subsequent operations, the probe operated properly.
Source record↗
The design and development of a miniature bi-stable latching solenoid valve for low thrust resistojets
The design approach and development demonstration are presented for a flightweight, miniature, magnetic latching shutoff valve, suitable for use with the ruggedized H2 and NH3 resistojet and the biowaste resistojet. The design criteria established provided for compatibility with specified ruggedized resistojet propellants as well as the biowaste and other propulsion system propellants.
Lynch, R. A.↗
Magnetic latching valve
Latching, fast-acting 2-port poppet valve has been developed for use in gas chromatograph - mass spectrometer combinations. Requisites included positive actuation time, few hundredths of a second, and static force holding valve in position at all times.
Conley, J. M.↗
Very high voltage latching relay
Relay consists of high voltage reed switch actuated by rotating permanent magnet mounted on stepper motor shaft, with actuation assembly isolated from high voltage circuit. Unit can be modified for use as double pole or double pole double throw latching relay and can be used in either air or vacuum.
Lovell, R. R.↗
Dual-action expanded-latch mechanism
Single drive actuator operates novel mechanism that expands, attaches to object, and withdraws to latch object firmly to another part. Packaging is extremely simple and compact, and eliminates need for machined parts or close tolerances.
Spencer, R. A.↗
Hatch latch mechanism for Spacelab scientific airlock
The requirements, design tradeoff, design, and performance of the Spacelab scientific airlock hatch latching mechanisms are described. At space side the hatch is closed and held against internal airlock/module pressure by 12 tangential overcenter hooks driven by a driver. At module side the hatch is held by 4 hooks driven by rollers running on a cammed driver.
Terhaar, G. R.↗