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Bensimon, M.

Publications and source records attributed to Bensimon, M..

Astronomical facilities for Spacelab

Three significant Spacelab facilities which are being developed, or planned by NASA will use the 1-2 week observational capability for attached payloads on Shuttle to carry out advanced astronomical observations in the ultraviolet visible, and infrared spectral regions during the decade of the 1980s. The three facilities are expected to evolve in capability over several Shuttle flights with a final objective of protracted observational capability from a permanent facility in space with periodic servicing and/or retrieval. The three facilities are the Office of Space Science package (OSS-3/7), the Solar Optical Telescope (SOT), and the Shuttle Infrared Telescope Facility (SIRTF). The scientific and technical objectives of these astronomical facilities include both their current and projected capabilities, their use of the manned Shuttle, and their eventual disposition to a long-term facility. International aspects of the missions, including General Investigator programs, are also being planned.

Reeves, E. M.

Capabilities offered by the Space Transportation System for the conduct of scientific experiments

The capabilities of the Space Transportation System (STS) to support the conduct of scientific investigations in space are reviewed for two modes of operation - dedicated Spacelab missions and mixed cargo missions. Along with these capabilities exist certain limitations. Their significance and NASA's approach for dealing with them are described. Examples of the unique aspects of the STS's capabilities are demonstrated by citing some of the investigations under development for early STS missions and others planned for future development. In addition, augmentation packages to increase STS capabilities are reviewed, and their impact on the conduct of future scientific investigations is projected.

Bensimon, M.

Predicting a vehicle's attitude response to a single yo despin

The method developed for analysis of single yo despin systems is a two step process. The first step utilizes the despin equations for a yo or yo-yo system to compute the cable tension force and its point of application on the body throughout the despin process. The second step considers the actual body configuration and treats the force just discussed as a prescribed external force acting on the surface of the body at the physical location of the despin system. The resulting vehicle coning angle is first computed using a digital computer program for a body with no initial coning prior to despin. Closed form solutions which utilize the previous results are then used to treat the effects of initial conditions.

Bensimon, M.