High-Resolution Charge-Coupled-Device Camera
800-by-800-element sensor and lens of 1.5-m focal length used in camera with 0.01-mrad resolution.
Engineering topics
Publications and source records attributed to Snyder, L. M..
800-by-800-element sensor and lens of 1.5-m focal length used in camera with 0.01-mrad resolution.
During January 1982 the NASA space transportation system will launch a Galileo spacecraft composed of an orbiting bus and an atmospheric entry probe to arrive at the planet Jupiter in July 1985. A prime element of the orbiter's scientific instrument payload will be a new generation slow-scan planetary imaging system based on a newly developed 800 x 800 charge-coupled device (CCD) image sensor. Following Jupiter orbit insertion, the single, narrow-angle, CCD camera, designated the Solid State Imaging (SSI) Subsystem, will operate for 20 months as the orbiter makes repeated encounters with Jupiter and its Galilean Satellites. During this period the SSI will acquire 40,000 images of Jupiter's atmosphere and the surfaces of the Galilean Satellites. This paper describes the SSI, its operational modes, and science objectives.
Momentum-velocity analyzer for measuring minute space particles
Photoheliograph study for Apollo telescope mount
Micrometeoroid detector-analyzer with ballistic pendulum for momentum measurement and capacitive foils for velocity