Development and construction of two hydrogen masers Interim technical report, 1 Feb. 1962 - 31 May 1963
Optimal construction of atomic hydrogen frequency standard for spacecraft application
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.
Optimal construction of atomic hydrogen frequency standard for spacecraft application
Multilayer metal deposition technique to provide electrical contacts for cadmium sulfide single crystals
Electronic circuitry for suspending electric vacuum gyro rotor in center of electrode sphere
Near-field solution for infinite line source above dielectric coated conducting plane
Sequential coding scheme for additive Gaussian channel with noisy feedback link
Reliability demonstration based on accelerated testing of overstressed components
Dynamic stability of eccentrically reinforced circular cylindrical shells
High speed digital computer program and data handling instructions for problem solving with structural analysis and interpretive system
Development of characteristic equations and error analysis for computer programs contained in structural analysis and matrix interpretive system
Preliminary study of alternate shift registers for eight-pole commutator
Astronaut performance during ingress-egress maneuvers through airlocks and passageways studied by water immersion simulation techniques
Lunar soil properties determination through simulation of rock grinding in ultrahigh vacuum
Experiment missions for OSO satellite rendezvous, capture, material retrieval, refurbishment, and extravehicular operation work
Systems support activities for planetary quarantine mission
Sterilizable ruggedized vidicon for lunar and planetary photography
Reactive sputtering and electron beam evaporation techniques for depositing glass coverslips on silicon solar cells
Integral valve and ram type electro-pneumatic actuator using onboard hydrogen supply for gimballing nozzle installation in J-2 rocket engine