Research on blunt-faced entry configurations at angles of attack between 60 deg and 90 deg
Stability and control of blunt reentry configurations at angles of attack between 60 and 90 degrees
SPACECRAFT CONFIGURATION↗
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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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Tabulated pressure data for a series of controls on a 60 deg. delta wing at mach numbers of 1.61 and 2.01
Performance test data for pressure distributions over 60 deg delta wing at Mach 1.61 and 2.01
DELTA WING↗
Design of a medium power dc to 115 volt, 60 Hertz ac inverter
Design of medium power dc to 115 volt, 60 Hertz ac inverter
POWER CONVERSION↗
Analysis of pressure distributions for a series of tip and trailing-edge controls on a 60 deg wing at Mach numbers of 1.61 and 2.01
Supersonic pressure distributions for tip and trailing edge controls on 60 deg delta wing
TRAILING EDGE↗
Low-speed Measurements of Oscillatory Lateral Stability Derivatives of a Model of 60 Deg Delta-wing Bomber
Low speed measurements of oscillatory lateral stability derivatives of 60 degree delta wing bomber model
BOMBER AIRCRAFT↗
Heat-transfer and pressure distributions on 60 deg and 70 deg swept delta wings having turbulent boundary layers
Heat-transfer and pressure distributions on 60 and 70 deg swept delta wings with turbulent boundary layers
PRESSURE DISTRIBUTION↗
Aerodynamic characteristics of a series of spherically blunted 10 deg cones with 30 deg and 60 deg base flares
Aerodynamic characteristics of slightly blunted conical bodies with 30 and 60 degree base flares
BLUNT BODY↗
60-day exposure to artificial atmospheres.
Hamsters, mice and rats exposed to elevated oxygen tensions for 60-day periods with nitrogen at high or minimal levels.
Environmental testing↗
An upper limit on the quiet time solar neutron flux at energies greater than 60 MeV
Upper limit on quiet time solar neutron flux at energies above 60 MeV determined by using balloon flights with Cerenkov scintillation counters
CERENKOV COUNTER↗
The effect of trailing-edge control deflection on the loading over a 60 deg delta-wing-body combination
Constant chord, trailing edge, control deflection effects on aerodynamic loading characteristics of 60 degree delta wing-body combination at transonic speeds
DELTA WING↗
Energy spectra of a number of celestial X-ray sources in the energy range from 2 to 60 kiloelectron volts.
Energy spectrum of X-ray source in Cygnus constellation with 2 to 60 kev
ENERGY SPECTRUM↗
An upper limit on the quiet time solar neutron flux at energies greater than 60 Mev.
New lower upper limit on solar neutron flux at energies greater than 60 mev for emission during quiet times
SOLAR RADIATION↗
Influence of Co super 60 gamma irradiation on the surface and bulk recombination rates in silicon.
Cobalt 60 gamma irradiation effects on P doped p- and n-type Si surface and bulk recombination rates
Lade, R. W.↗
Evaluation of a closed-cycle life-support system during a 60-day manned test.
Closed cycle life support system 60-day manned test in space cabin simulator noting water and oxygen recovery, thermal control, atmosphere control, etc
Bonura, M. S.↗
Meteorological rocket research since 1959 and current requirements for observations and analysis above 60 kilometers
Survey of rocket soundings to 60 km, and 100 km
Quiroz, R. S.↗
Performance characteristics from Mach 2.58 to 1.98 of an axisymmetric mixed-compression inlet system with 60-percent internal contraction
Performance test from Mach 2.58 to 1.98 of axisymmetric mixed-compression inlet system with 60 percent internal contraction
Cubbison, R. W.↗
Wind tunnel investigation of the flow field under a 60 degree swept wing at Mach numbers from 0.6 to 2.6
Wind tunnel studies of flow field under 60 deg swept wing from Mach 0.6 to 2.6
Blaha, B. J.↗
The 3d yields 2p pionic transition in Ni 258 and Ni 60
Pionic X rays in nickel 58 and 60
Jenkins, D. A.↗