Flight characteristics of a wingless rocket- powered model with four externally mounted air-to-air missiles at Mach numbers 0.7 to 1.6
Explore the source record for details and available documents.
Brown, C. A., Jr.↗
SEARCH · Engineering Papers
Results for “mount”
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.
Development of the flame sprayed aluminum concept for conductive cooling of XE engine- mounted electrical cables, April 1964 - October 1966
Explore the source record for details and available documents.
Sita, E. R.↗
Self-forming shim or gasket for mounting heavy equipment
Soft, cross-serrated aluminum shims are used as mating gaskets between uneven surfaces. Under pressure, the aluminum flows to conform with surface irregularities, forming a plane of uniform bearing.
Walter, G. W.↗
Proton sensitivity of films used in Apollo Telescope Mount satellite missions
Proton sensitivity of films used in ATM satellite missions
Potter, R. A.↗
Interactions between a hypersonic neutral gas beam and an orificed pressure gauge mounted in a spinning satellite
Interactions between hypersonic neutral gas beam and orificed pressure gauge in spinning satellite noting dependence on angle of attack
Newton, G.↗
Prevention of damage to delicate connectors during mounting of heavy engines for testing
Air-bearing-pad principle, combined with monitoring system of the air-bearing force, prevents damage between electrical and mechanical connectors joining a large engine system to the test stand during remote mating. Pad provides a cushion between engine and test stand.
Hendrickson, R. J.↗
Spectral Hygrometry Program, Mount Hopkins, Arizona - Instrumentation and Procedure Manual
Measuring total precipitable water vapor and correlations between water vapor and local meteorological parameters
Vaughn, C. R.↗
A meteorological report for the Mount Hopkins Observatory - 1968 - 1969
Meteorological data for Mt. Hopkins Observatory for 1968 and 1969
Goodwin, K.↗
The Hekla fires - A preliminary report of the 1970 Mount Hekla volcanic eruption. A report from the Smithsonian Insitution Center for Short-Lived Phenomena, 15 June 1970
Describing eruption in region of Mt. Hekla, Iceland and toxic hazards from volcanic ash
Thorarinsson, S.↗
Solar cell mounting Patent
Fabrication of solar cell banks for attaching solar cells to base members or substrates
Forehand, L.↗
Flight investigation of a V/STOL transport model having six wing-mounted lift fans
Free flight tests in hoovering and forward flight free flight tests in hovering and forward flight lift fans
Grafton, S. B.↗
Critical speeds of a rotor in rigidly mounted, externally pressurized, air-lubricated bearings
Calculation of rotor critical speeds for two bearing rotor system from rigid body theory using film stiffness as determined from zero speed, load eccentricity data
Cunningham, R. E.↗
Medical problems at high altitude sites and the Mount Logan, Yukon, High Camp
Medical aspects of high altitude environments including hypoxia at Logan High Camp
Rennie, I. D.↗
Active regions. I - The occurrence of solar flares and the development of active regions. II - Mount Wilson 16997- A small spot with big flares
Solar active regions, examining development and occurrence of solar flares
Zirin, H.↗
Experimental investigation of the performance of vortex generators mounted in the supersonic portion of a mixed-compression inlet
Vortex generators were investigated as a means of controlling the throat boundary layer in a Mach 2.5 mixed-compression inlet. With or without throat bleed, the generators were unable to produce the inlet peak recoveries available with good performance bleed. Generators placed on the unbled inlet centerbody ahead of the cowl shock impingement point degraded inlet performance. Generators placed further aft on the unbled centerbody, but ahead of the throat, improved inlet performance at conditions where the terminal shock could cause boundary layer separation. Adding generators to the inlet with throat bleed reduced performance. Bleed aft of the generators degraded the vortex flow field.
Michell, G. A.↗
Aerodynamic characteristics of the North American Rockwell space shuttle delta-wing orbiter (110C) alone and with belly-mounted external oxygen/hydrogen tanks (M equals 0.6 to 5.0)
Experimental aerodynamic investigations were conducted at the MSFC 14 x 14 inch trisonic wind tunnel on a .0044 scale model of the space shuttle orbiter, 110C. The test configurations included the orbiter alone and with external oxygen/hydrogen belly tanks. The six component aerodynamic force and moment data obtained cover a Mach number range from 0.6 to 4.96 at angles of attack from 10 to 60 deg at 0 deg sideslip angle and -10 to 10 deg at -6 deg sideslip angle. Reynolds number per unit length varied somewhat with Mach number but was a nominal 6.8 million per foot.
Allen, E. C.↗
Lava tubes of the Cave Basalt, Mount St. Helens, Washington.
Explore the source record for details and available documents.
Greeley, R.↗
Strain arrestor plate for mounting rigid insulating tiles
Plate is made of material having coefficient to thermal expansion similar to that of insulating material. Although plate may be formed from appropriate alloy, it has been found that a combination of graphite fibers in epoxy resin is satisfactory and much lighter in weight.
Kural, M. H.↗