Infrared spectroscopy experiment for Mariner Mars 1971
IR Michelson interferometer for Mariner Mars 1971 mission, investigating atmospheric and surface temperatures and atmospheric water vapor content
Engineering topics
Publications and source records attributed to Hanel, R. A..
IR Michelson interferometer for Mariner Mars 1971 mission, investigating atmospheric and surface temperatures and atmospheric water vapor content
Infrared interferometer spectrometer for Mariner spacecraft in Mars orbit
Numerical model applied to Venus atmosphere above cloud region to determine radiative-convective equilibrium temperatures
Michelson type interferometer for Nimbus meteorological satellite to obtain vertical temperature, humidity and ozone profile
Michelson interferometer to obtain vertical temperature and humidity profile from Nimbus satellite
Michelson type interferometer for Nimbus meteorological satellite to obtain vertical temperature, humidity and ozone profile
Gaseous composition of unknown planetary atmosphere determined, using acoustic experiment combined with pressure and temperature data
Equilibrium temperature distribution, thermal emission, and limb function computed for Venus cloud cover model
IRIS - infrared interferometer spectrometer measurements of atmosphere vertical structure - humidity, temperature, and cloud height
Radiative equilibrium in planetary atmospheres - application of strong line absorption law to atmosphere of venus
Mars surface and atmosphere characteristics from thermal emission spectrum measurement by infrared interferometer on planetary flyby spacecraft
Infrared horizon of planet earth - difference between surface, atmospheric, & outer space spectral regions - choosing spacecraft sensors
Discussion of future experiments concerning ir radiation, cloud top heights, solar constants and atmospherics, proposed for meteorological satellites
Investigation of the discontinuity between the earth, the atmosphere and outer space in the structure of the infrared horizon
TIROS II contains instrumentation for measuring infrared and reflected solar radiation from the earth and its atmosphere. A medium resolution scanning radiometer and a low resolution non-scanning radiometer are employed. The satellite's spin provides the scan line of the medium resolution radiometer which is then advanced by the orbital motion. The spatial resolution is about 40 miles square when the earth directly beneath the satellite is viewed. The five channels employ bolometer detectors and filters to limit the spectral responses to five bands: 6 to 6.5 microns, 8 to 12 microns, 0.2 to 6 microns, 8 to 30 microns, and 0.55 to 0.75 microns. These five bands study, respectively: radiation in the water vapor absorption band; day and nighttime cloud cover; albedo; thermal radiation; and visual maps for comparison with satellite vidicon pictures. The low resolution non-scanning radiometer measures the earth's black-body temperature and albedo. Its field when viewing directly below is a circle of 450 miles diameter, covering part of each frame from the wide-field television camera. This radiometer consists of two thermistors, each in the apex of a reflective cone which provides optical gain. One thermistor is black and responds to both thermal and reflected solar radiation. The second responds to thermal but reflects solar radiation. The design, calibration, performance, and data reduction for both systems are discussed herein.
The TIROS II meteorological satellite was placed into orbit on November 23, 1960. It contains two television cameras and equipment for a family of electromagnetic radiation experiments, including a medium resolution radiometer. The medium resolution radiometer is a cluster of five sensors which have their optical axes inclined 45 deg. to the spin axis of the satellite. The spin of TIROS II provides the scanning motion. The five radiometer channels are sensitive to the following spectral bands: 6 to 6.5; 8 to 12; 0.2 to 6; 8 to 30; and 0.55 to 0.75 microns.
The blackbody temperature and the albedo of a planet, and the variation of both parameters with latitude, longitude, and time, are of great value in understanding the climatic and meteorological conditions of the planet. An unchopped radiometer with a wide but restricted field of view is capable of such temperature and albedo measurements. Coated thermistors mounted in highly reflective cones serve as detectors. Their performance as sensor elements is analyzed in detail herein to prove the feasibility of the measurement. The simplicity of the instrumentation and the low information bandwidth required make the experiment equally attractive for earth satellites and space probes.
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