Flight-determined low-speed lift and drag characteristics of the lightweight m2-f1 lift- ing body
Flight-determined low speed lift and drag characteristics of lightweight M-2 lifting body
LIFT↗
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Evaluation of the lateral-directional stability and control characteristics of the lightweight m2-f1 lifting body at low speeds
Lateral directional stability and control characteristics of lightweight M2-F1 lifting body at low speeds
LATERAL STABILITY↗
Development of a lightweight external insulation system for liquid-hydrogen stages of the saturn v vehicle.
Lightweight external insulation system for liquid hydrogen stages of Saturn V vehicle
CRYOGENIC STORAGE↗
Solar cell submodule design facilitates assembly of lightweight arrays
Solar cell submodules with bus bars that leave tabs along one end of the submodule and wires with raised portions along the other end are assembled by interlocking the tabs and wires of adjacent submodules. This structural design is lightweight and reliable and requires no metallic substructure.
Yasui, R. K.↗
Portable lightweight cell provides controlled environment
Inflatable, lightweight cell provides a separate, secondary environment for a spacesuited man in case of spacesuit damage or malfunction. The cell has a pressure-sealing zipper and is equipped to maintain a livable atmosphere.
Shelton, S.↗
Lightweight, all-metal hose assembly has high flexibility and strength over wide range of temperature and pressure
Lightweight flexible, metal braid reinforced hose assembly is used in high and low pressure oxygen, helium, and hydrogen systems. These hose assemblies have been successfully used on the Saturn-2 stage to provide joints of sufficient flexibility to absorb movement resulting from temperature variations.
Bessing, L. L.↗
Fabrication of lightweight parabolic concentrators from a glass master Final report
Forming of optical lightweight solar concentrator on glass master - spray technique for resin substrate layers
SOLAR COLLECTOR↗
Development of lightweight thermal insulation materials for rigid heat shields Summary report no. 1, Jun. 25, 1964 - Jun. 25, 1965
Ceramic foam as lightweight thermal insulation for rigid heat shields in launch vehicles
HEAT SHIELD↗
Supersonic aerodynamic heating tests on a lightweight external insulation system for liquid-hydrogen tanks of boost vehicles
Supersonic aerodynamic heating tests on external lightweight insulation system for liquid hydrogen tanks of boost vehicles
ROCKET BOOSTER↗
Development of high-performance lightweight electrodes for hydrogen-oxygen fuel cells Third quarterly report, 6 Oct. 1965 - 5 Jan. 1966
High performance, lightweight electrodes for hydrogen-oxygen fuel cells
ELECTRODE↗
Development of lightweight rigid solar panel Interim design report, 1 Jan. - 30 Apr. 1966
Lightweight rigid photovoltaic solar panel
PHOTOVOLTAIC CELL↗
Development of a lightweight cryogenic insulating system Final report, 30 Jun. 1964 - 31 May 1966
Lightweight external panel insulation systems for thermal protection of cryogenic launch vehicle propellant tanks
PROPELLANT TANK↗
Stability and control characteristics at a Mach number of 1.89 of a lightweight glider reentry configuration
Stability and control characteristics at supersonic speeds of lightweight reentry glider with diamond-wing planform
WING PLANFORM↗
Investigation of a lightweight self-evacuating prefabricated multi-layer insulation system for cryogenic space propulsion stages Final report, 3 Jun. 1965 - 31 Jul. 1966
Lightweight self-evacuating prefabricated multilayer insulation system for cryogenic space propulsion stages
MULTILAYER STRUCTURE↗
Fabrication of lightweight turbine components using electron-beam welding for the attachment of sheet metal blades to discs and shrouds
Fabrication of lightweight turbine components for M-1 engine oxidizer turbopump using electron beam welding for attaching sheet metal blades to discs and shrouds
TURBOPUMP↗
The development and testing of a lightweight flight prototype ion engine system.
Lightweight flight prototype mercury ion engine system development and testing
ION ENGINE↗
Lightweight inflatable shadow shields for cryogenic space vehicles.
Lightweight inflatable shadow shields for cryogenic space vehicles and performance in conjunction with superinsulation
THERMAL INSULATION↗
Lightweight power-conditioning system for ion engines using energy-storage transformers for conversion, nondissipative regulation and protection.
Lightweight power-conditioning system for ion engines using energy-storage transformers for conversion, nondissipative regulation and protection
TRANSISTOR↗