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Exploring the Unknown - NASA's History Office

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EXPLORING THE UNKNOWN 239<br />

terometer radars, passive microwave radiometers, and UV line scanners in 1965 and plan<br />

to add more advanced multispectral cameras, metric and panoramic cameras, more<br />

advanced infrared scanners, infrared spectrometers and passive microwave imagers in<br />

1966. The studies and <strong>the</strong> aircraft program are planned to be carried out on a continuing<br />

basis to provide for economical testing of instrumentation over sites of known characteristics<br />

prior to orbital testing.<br />

As a result of <strong>the</strong>se activities <strong>the</strong> user community has identified and specified candidate<br />

instruments for orbital test. The initial and most urgent of <strong>the</strong>se are a wide range<br />

spectral scanner (0.3–13 microns) covering <strong>the</strong> near UV, visible and part of <strong>the</strong> IR spectrum<br />

(190 meter resolution) and a multispectral synoptic photographic system (of<br />

approximately 30 meters resolution). NASA is currently planning incorporation of <strong>the</strong>se<br />

instruments into an already planned flight in 1969.<br />

A ra<strong>the</strong>r completely instrumented natural resources satellite is being considered for<br />

flight in 1970 or 1971 involving <strong>the</strong> following instruments:<br />

Metric Cameras<br />

Panoramic Cameras<br />

Multispectral Tracking Telescope<br />

Multispectral Synoptic Cameras<br />

Imaging Radars (8.0 gc)<br />

Radar Altimeter/Scatterometers (0.4 and 0.8 gc)<br />

Wide Range Spectral Scanner (0.3–13 microns)<br />

Infrared Long Wavelength Spectrometer (18–16 microns)<br />

Infrared Short Wavelength Spectrometer (0.4–2.5 microns)<br />

Infrared Radiometer (10–12 microns)<br />

Passive Microwave Imager (9.0 gc)<br />

Passive Multichannel Microwave Radiometers (0.4–21 cm)<br />

UV Imaging Spectrometer (3900–4900 Angstroms and 5800–6800 Angstroms)<br />

Laser Altimeter/Scatterometer<br />

Absorption Spectrometer (UV, visible, IR)<br />

Chirp Radar System (75–450 mc’s)<br />

Gravity Gradiometer<br />

Magnetometer System (triaxial fluxgate and rubidium vapor)<br />

Flight test of this entire group of instruments simultaneously is highly desirable<br />

because <strong>the</strong> cross correlation of data from various portions of <strong>the</strong> electromagnetic spectrum<br />

acquired under similar lighting and wea<strong>the</strong>r conditions will yield far more information<br />

than data acquired at separate times by individual instruments.<br />

If successful and needed, a repeat of this satellite is being considered for flight in<br />

1971–72 to continue <strong>the</strong> development of <strong>the</strong> technology and <strong>the</strong> ability to handle and<br />

analyse [sic] accumulated data.<br />

[3] Orbital Requirements<br />

During <strong>the</strong> experimental phase of this program (pre-1975) <strong>the</strong> natural resource users<br />

require data to be collected periodically over a number of natural and cultural resources<br />

test sites. These sites must be readily accessible and available for study by well trained scientists.<br />

Many of <strong>the</strong> sites essential to this program fall within <strong>the</strong> United States both<br />

because of <strong>the</strong> subject matter involved (such as land use in metropolitan areas, water pollution<br />

in Great Lakes, water resources in nor<strong>the</strong>ast and arid west, geo<strong>the</strong>rmal power sites<br />

in Pacific Northwest etc.) and because of <strong>the</strong> ready availability of trained personnel for<br />

ground control studies. Orbital inclinations of at least 480 are <strong>the</strong>refore extremely important<br />

during <strong>the</strong> experimental phases of this program. It should be emphasized however,

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