Performance of ATS Spin-Scan Cloudcover Camera /SSCC/ equipment at Mojave ground station. ATS project
Performance of ATS 1 spin-scan cloud cover camera equipment at Mojave ground station
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Performance of ATS 1 spin-scan cloud cover camera equipment at Mojave ground station
Automatic underwater camera system design and performance characteristics for time lapse photography of algae growth and sedimentation
Returned Surveyor 3 camera visor examined for alpha radioactive deposit formed by decay of radon isotopes diffusing out of lunar surface
Solid state television camera system consisting of monolithic semiconductor mosaic sensor and molecular digital readout systems
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Longitudinalfilm gate and lock mechanism for securing film in motion picture cameras under vibration and high acceleration loads
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Determination of black and white lunar television camera performance after long storage for Apollo program
Design and characteristics of laser camera system with diffusion filter of small particles with average diameter larger than wavelength of laser light
Appendices to engineering evaluation tests of Surveyor 3 television camera returned from moon by Apollo 12 astronauts - Vol. 2
In-flight calibration of 500-mm Hasselblad camera flown on Apollo 14
Mariner Mars 1969 TV cameras instrument design and calibration techniques
Folded all-reflecting Schmidt camera UV image converter system for space astronomy applications, discussing pressure sensitivity effects on UV direct recording emulsion
Vibration effects on image resolution and acutance of Zeiss RMK AR 15/23 aerial camera, using aircraft vibration simulator for testing
Alpha radioactivity in Surveyor 3 camera visor, calculating upper limit of Po 210 at equilibrium of Oceanus Procellarum
Compact, lightweight camera which advances film frames without use of conventional sprockets and slip clutches obtains time lapse photomicrographs of human cell growth in a zero-G environment over a period of about a month.
The f1 Hewitt camera is a field flattened Schmidt system of 60cm aperture. The salient features of this equipment are briefly described. Details of the methods of plate measurement are then given. The plate reduction is carried out in two stages. The plate is first calibrated using the photogrammetric method. The formulae usually quoted have been extended to take account of the large distortion introduced by the field flattening lens. In the second stage, the satellite measurements are reduced to satellite positions corrected for refraction, aberration, and when necessary, phase.
A sensor system which provides registered high-solution multispectral images from a single sensor with no mechanical moving parts is reported, and the operation of an image dissector camera (IDC) is described. An earth scene 100 nautical miles wide is imaged through a single lens onto a photocathode surface containing three spectral filters, thereby producing three separate spectral signatures on the photocathode surface. An electron image is formed, accelerated, focused, and electromagnetically, deflected across an image plane which contains three sampling apertures, behind which are located three electron multipliers. The IDC system uses electromagnetic deflection for cross-track scanning and spacecraft orbit motion for along-track scanning, thus eliminating the need for a mechanical scanning mirror.