Space environment simulator test program. Volume 2 - Unmanned thermal performance evaluation of a Gemini extravehicular space suit Test report, May 1965
Temperature data plots of Gemini Bravo series space suit tests
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Temperature data plots of Gemini Bravo series space suit tests
Meteorological wind, and temperature data from atmospheric radiosonde soundings in Southern Hemisphere
Ablation and temperature data for Apollo heat shield material using Pacemaker vehicle for flight test
Small scale wind and temperature structure from wind and temperature data from Japanese MT 135 and American ARCAS meteorological rocket systems
Mariner Venus and Mars spacecraft flight temperature data compared with space simulator thermal test results
Vertical wind velocities, rotation, and generation of Martian dust devils, and Martian atmospheric temperature data
Error analysis of high resolution balloon-borne temperature sensor and comparison of temperature data with simultaneous rawinsonde measurements
Bidirectional reflectance of solar radiation and IR temperature data from Nimbus 2 satellite to differentiate clouds above snow surfaces
Winter diurnal behavior of northern high latitude ionospheric electron density using temperature data from Langmuir probes
Oxygen pressure, volume and temperature data and derived thermodynamic properties presented in tabular form
Stark-broadened neutral atomic line widths and shifts, determining electron densities from H beta profiles and pressure-temperature data
Liquid and gaseous oxygen difluoride compatibility tests with plastic and metal orifices and metal ignition temperature data
Ionospheric electron and nitrogen density and temperature data from thermospheric soundings during 7 Mar. 1970 total solar eclipse
Gum Nebula size, density and electron temperature data from RAE-1 and OGO-5 satellites and ground based telescopes observations, correlating with Vela X supernova outburst
The Jimsonde, a high-resolution lightweight temperature sensor developed for use with the FPS-16 Radar/Jimsphere wind system, and its related systems are discussed; and an error analysis that shows the sonde to have an rms error of 0.41 C at sea level and 0.56 C at 18 km is presented. Five flight tests, a sequence of four tests and one individual test, of the Jimsonde were made. For comparative purposes, radiosonde temperature data are presented along with the Jimsonde data.
The Raman shifted return of a lidar system was utilized to make atmospheric temperature measurements. The measurements were made along a horizontal path at temperatures between -20 and +30 C and at ranges of about 100 meters. The temperature data were acquired by recording the intensity ratio of two portions of the rotational Raman spectrum which were simultaneously sampled from a preset range. Measurements were made to an accuracy of + or - 3 C with 1 minute temporal resolution.
A position sensitive detector was made using the lithium diffused layer of a lithium-drifted-silicon detector as the uniform resistive layer. An expression is derived for estimating the resistance from the thickness of the lithium layer. Expressions for the noise and ballistic deficit for single differentiation-double integration pulse shaping are presented. Room temperature data for a 1 Mev proton beam on a 45 mm long detector shows that the linearity is better than .05% and that the position resolution is 1.06 + or - .05 mm.
Results are presented of CO2 extinction coefficient measurements that were performed under conditions of temperature and pressure different from those used by previous investigators. The results show that, whereas pressure effects are generally negligible, temperature dependence is strong enough to invalidate the use of room temperature data for the Mars atmosphere.