Gravitation Research

Contains reports on one research project.Joint Services Electronics Program (Contract DAAB07-71-C-0300)National Aeronautics and Space Administration (Grant NGR 22-009-526

Gravitation Research

Contains reports on two research projects.Joint Services Electronics Programs (U.S. Army, U. S. Navy, and U. S. Air Force) under Contract DAAB07-71-C-0300National Aeronautics and Space Administration (Grant NGR 22-009-526)National Science Foundation (Grant GP-24254

Gravitation Research

Contains research objectives and summary of research.Joint Services Electronics Programs (U. S. Army, U. S. Navy, and U. S. Air Force) under Contract DAAB07-71-C-0300National Aeronautics and Space Administration (Grant NGR 22-009-526)National Science Foundation (Grant GP-24254

Optical and Infrared Spectroscopy

Contains report on one research project.Joint Services Electronics Programs (U. S. Army, U. S. Navy, and U. S. Air Force) under Contract DA 28-043-AMC-02536(E)U. S. Air Force (ESD Contract AF 19(628)-6066)M. I. T. Sloan Fund for Basic Researc

Parachute Swivel Mechanism for planetary entry

A parachute swivel mechanism (PSM) for planetary entry missions such as a Mars probe (MARSNET) or return of cometary material samples (ROSETTA mission) has been developed. The purpose of the PSM is to decouple the spin of the probe from the parachute, with low friction torque, during both the deployment and descent phases. Critical requirements are high shock loads, low friction, low temperatures, and several years of storage in the deep space environment (during the cruise phase of the probe, prior to operation). The design uses a main thrust ball bearing to cope with the load requirement and a smaller thrust ball bearing for guiding of the shaft. Except for use on the Viking and Galileo swivels, it appears that this type of bearing has very rarely been employed in space mechanisms, so that little is known of its friction behavior with dry lubrication. A slip ring assembly allows the transfer of electrical power for post-reefing of the parachute. A test program has been conducted covering the environmental conditions of Mars entry and Earth reentry. This paper describes requirement constraints, model missions of planetary entries, a bearing trade-off, analyses performed, design details, the lubrication system, and test results (friction torque versus load/spin rate). In addition, the design of the test rig is addressed

Infrared Nonlinear Optics

Contains reports on one research project.U.S. Air Force - Office of Scientific Research (Grant AFOSR-76-2894

Gravitation Research

Contains research objectives and summary of research.National Aeronautics and Space Administration (Grant NGR 22-009-526)Joint Services Electronics Program (Contract DAAB07-71-C-0300

Infrared Instrumentation and Astronomy

Contains research objectives and summary of research on four research projects.Joint Services Electronics Program (Contract DAAB07-75-C-1346)National Aeronautics and Space Administration (Grant NGR 22-009-526)National Aeronautics and Space Administration (Contract NAS5-22828

Infrared Instrumentation and Astronomy

Contains research objectives and summary of research on five research projects.Joint Services Electronics Program (Contract DAAB07-76-C-1400)M.I.T. Sloan Fund for Basic ResearchNational Aeronautics and Space Administration (Contract NAS5-23731)National Aeronautics and Space Administration (Grant NGR 22-009-526

Infrared Instrumentation and Astronomy

Contains reports on one research project.Joint Services Electronics Program (Contract DAAB07-75-C-1346