A discussion is presented regarding valves which can be cycled repeatedly and are available from industry for application in the inlet system for the Pioneer Venus Probe mass spectrometer. Both solenoid type and latching type valves are considered. The study is divided into two principal areas: (1) preparation of a valve specification reflecting the requirements of the inlet system cyclic valves for the Pioneer Venus Probe mass spectrometer and the submittal of this specification to potential valve suppliers for their response and proposal; (2) preparation of a design layout of an optimum cyclic valve meeting all of the valve specification requirements
Fabrication and acceptance testing, fluorine compatibility testing, valve refurbishment and testing,...
Improvement of heat transfer efficiency of the spacecraft thermal control subsystem constitutes a re...
The present invention is a space vehicle valve system which controls the internal pressure of a spac...
The development of the in-house Miniaturized Double Latching Solenoid Valve, or Microvalve, for the ...
A survey of mechanical vacuum pumps was completed. A small Roots blower for flight mass spectrometer...
NASA's participation in the multi-nation ExoMars 2018 Rover mission includes a critical astrobiology...
Recent performance concerns involving the Space Shuttle Main Engine Propellant Valve Actuator assemb...
Marshall Space Flight Center (MSFC) has developed a valve concept to replace traditional pyrotechnic...
The articles in this Compilation will be of interest to mechanical engineers, users and designers of...
Valve concept evaluation, final candidate selection, design, manufacture, and demonstration testing ...
Tester investigates fundamental factors affecting cyclic life and sealing performance of valve seats...
Mission Research Corporation (MRC) in cooperation with the Jet Propulsion Laboratory (JPL) has devel...
Two way, latching, dc solenoid valve to isolate reaction control engine clusters from main hypergoli...
Monograph reviews and assesses current design practices, and from them establishes firm guidance for...
Low leakage rate, large diameter vent and relief valve operates satisfactorily over a large temperat...
Fabrication and acceptance testing, fluorine compatibility testing, valve refurbishment and testing,...
Improvement of heat transfer efficiency of the spacecraft thermal control subsystem constitutes a re...
The present invention is a space vehicle valve system which controls the internal pressure of a spac...
The development of the in-house Miniaturized Double Latching Solenoid Valve, or Microvalve, for the ...
A survey of mechanical vacuum pumps was completed. A small Roots blower for flight mass spectrometer...
NASA's participation in the multi-nation ExoMars 2018 Rover mission includes a critical astrobiology...
Recent performance concerns involving the Space Shuttle Main Engine Propellant Valve Actuator assemb...
Marshall Space Flight Center (MSFC) has developed a valve concept to replace traditional pyrotechnic...
The articles in this Compilation will be of interest to mechanical engineers, users and designers of...
Valve concept evaluation, final candidate selection, design, manufacture, and demonstration testing ...
Tester investigates fundamental factors affecting cyclic life and sealing performance of valve seats...
Mission Research Corporation (MRC) in cooperation with the Jet Propulsion Laboratory (JPL) has devel...
Two way, latching, dc solenoid valve to isolate reaction control engine clusters from main hypergoli...
Monograph reviews and assesses current design practices, and from them establishes firm guidance for...
Low leakage rate, large diameter vent and relief valve operates satisfactorily over a large temperat...
Fabrication and acceptance testing, fluorine compatibility testing, valve refurbishment and testing,...
Improvement of heat transfer efficiency of the spacecraft thermal control subsystem constitutes a re...
The present invention is a space vehicle valve system which controls the internal pressure of a spac...