The final report for the automatic exposure control study for space sequential cameras, for the NASA Johnson Space Center is presented. The material is shown in the same sequence that the work was performed. The purpose of the automatic exposure control is to automatically control the lens iris as well as the camera shutter so that the subject is properly exposed on the film. A study of design approaches is presented. Analysis of the light range of the spectrum covered indicates that the practical range would be from approximately 20 to 6,000 foot-lamberts, or about nine f-stops. Observation of film available from space flights shows that optimum scene illumination is apparently not present in vehicle interior photography as well as in vehi...
The methods of measuring the existence of erosion and the effects of sand stabilization control syst...
Advanced studies are reviewed. Atmospheric sciences, magnetospheric physics, solar physics, gravitat...
The performance of satellite subsystems and the response of in-orbit payload systems are summarized....
Six scientific objectives/experiments were derived which consisted of agriculture/forestry/range res...
Restructuring research objectives from a technical readiness demonstration program to an investigati...
The design of the high resolution imager (HRI) on HEAO 2 was modified for use in the instrument comp...
Visual system parameters and stereoptic television component geometries were evaluated for optimum v...
A flight experiment designed to demonstrate current cryogenic heat pipe technology was defined and e...
A physiological date telemetry system, consisting basically of a portable unit and a ground base sta...
The feasibility of classifying an airport terminal area for multipath effects, i.e., fadeout potenti...
Data sheets are presented for 11 internal payloads, 30 externally mounted payloads, and 46 free flye...
Test program for determining visual reference requirements for pilot control of gliding parachutes u...
The reusable design of the Space Shuttle requires a target life of 7.5 hours for the turbopumps of t...
A set of hardware similar to the SEASAT A configuration requirement, suitable for installation and o...
Pressure and heat transfer tests were conducted simulating flight conditions which the space shuttle...
The methods of measuring the existence of erosion and the effects of sand stabilization control syst...
Advanced studies are reviewed. Atmospheric sciences, magnetospheric physics, solar physics, gravitat...
The performance of satellite subsystems and the response of in-orbit payload systems are summarized....
Six scientific objectives/experiments were derived which consisted of agriculture/forestry/range res...
Restructuring research objectives from a technical readiness demonstration program to an investigati...
The design of the high resolution imager (HRI) on HEAO 2 was modified for use in the instrument comp...
Visual system parameters and stereoptic television component geometries were evaluated for optimum v...
A flight experiment designed to demonstrate current cryogenic heat pipe technology was defined and e...
A physiological date telemetry system, consisting basically of a portable unit and a ground base sta...
The feasibility of classifying an airport terminal area for multipath effects, i.e., fadeout potenti...
Data sheets are presented for 11 internal payloads, 30 externally mounted payloads, and 46 free flye...
Test program for determining visual reference requirements for pilot control of gliding parachutes u...
The reusable design of the Space Shuttle requires a target life of 7.5 hours for the turbopumps of t...
A set of hardware similar to the SEASAT A configuration requirement, suitable for installation and o...
Pressure and heat transfer tests were conducted simulating flight conditions which the space shuttle...
The methods of measuring the existence of erosion and the effects of sand stabilization control syst...
Advanced studies are reviewed. Atmospheric sciences, magnetospheric physics, solar physics, gravitat...
The performance of satellite subsystems and the response of in-orbit payload systems are summarized....