Stage sizing data for an unmanned planetary sample return mission, task E-94 Project technical report
Outbound and inbound stage weight requirements for planetary sample return mission payload and energy requirements - graphs
Gilbertson, R. D.↗
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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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Effect of engine position and high-lift devices on aerodynamic characteristics of an external-flow jet-flap STOL model
Effect of engine position and high lift devices on aerodynamic characteristics of external flow, jet flap STOL model - graphs
Smith, C. C., Jr.↗
Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6
Wind tunnel investigation of hypersonic transport model aerodynamic characteristics at Mach numbers to 6 - graphs
Ellison, J. C.↗
Low-subsonic longitudinal aerodynamic characteristics of a twin-body space-shuttle booster configuration
Low subsonic longitudinal aerodynamic characteristics of twin body space shuttle booster configuration using low turbulence pressure tunnel - graphs
Spencer, B., Jr.↗
Study of the effect of spacecraft window configuration on lines of sight
Pressure deformations of spacecraft windows and angular line-of-sight deviations of light rays from these windows causing errors in celestial navigation sightings - graphs
Kelley, D. M.↗
Evaluation of metabolic losses in whole body sweat from measurements of small skin areas
Tables and graphs of metabolic losses in whole body sweat determined by small skin area measurements
Van Beaumont, W.↗
Spectra of reflected solar energy 0.4 to 2.4 microns - Clouds, snow, fields
Spectra of reflected solar energy from clouds, snow, and fields at 0.4 to 2.4 microns using C-47 and B-57B aircraft - graphs
Blaine, L. R.↗
Compendium of modal densities for structures
Expressions and graphs for estimating average modal densities for various structural elements of engineering importance including beams, rods, circular plates, and conical shells
Hart, F. D.↗
Full-scale wind tunnel tests of a low-wing, single-engine, light plane with positive and negative propeller thrust and up and down flap deflection
Full scale wind tunnel tests of low wing, single engine, light aircraft with positive and negative propeller thrust and up and down flap deflection - graphs
Morris, J. J.↗
Model tests of concepts to reduce hot gas ingestion in VTOL lift engines
Model tests of concepts to reduce hot gas ingestion in VTOL lift engines in low and cross wind conditions - graphs
Hall, G. R.↗
Wind-tunnel investigation of an external-flow jet-flap transport configuration having full-span triple-slotted flaps
Wind tunnel investigation of external-flow jet-flap transport configuration having full-span tripple-slotted flaps - graphs
Parlett, L. P.↗
Feasibility study of a radiator and power divider for 50 - 60 GHz phased array
Feasibility study of radiator and power divider for 50 to 60 GHz phased array - graphs
Green, K. A.↗
Evaluation of ion density and plasma potential from Langmuir probe data
Evaluation of ion density and plasma potential from Langmuir probe data - graphs
Krawec, R.↗
Calculated pressure distributions and components of total-drag coefficients for 18 constant-volume, slender bodies of revolution at zero incidence for Mach numbers from 2.0 to 12.0, with experimental aerodynamic characteristics for three of the bodies
Pressure distributions and drag coefficients of 18 constant length and volume slender bodies of revolution at zero incidence for Mach numbers 2.0 to 12.0 - graphs
Stivers, L. S., Jr.↗
Van Allen belt radiation on Tiros/TOS/ITOS spacecrafts
Van Allen belt radiation on Tiros/TOS/ITOS spacecrafts - graphs
Stassinopoulos, E. G.↗
Space shuttle: Subsonic longitudinal and lateral-directional stability investigation of the MDAC LCR orbiter, unpowered and powered
Subsonic longitudinal and lateral directional stability investigation of MDAC LCR orbiter, unpowered and powered - graphs
Mann, R.↗
Dynamic analysis, with feedback characterization, of hybrid human musculo- skeletal frameworks by the linegraph-flowgraph procedure
Dynamic response with feedback characterization of human musculoskeletal frameworks by linegraph- flow graph procedure
Ghista, D. N.↗
Insulating effectiveness of self-spacing dimpled foil
Experimental data are graphed for determining conductive heat losses of multilayer insulation as function of number of foil layers. Foil was 0.0051 cm thick Nb, 1% Zr refractory alloy, dimpled to 0.0254 cm with approximately 28 dimples/sq cm. Heat losses were determined at 0.1 microtorr between 700 and 1089 K.
Bond, J. A.↗