Photograph used for a newspaper owned by the Oklahoma Publishing Company.

Photograph used for a story in the Daily Oklahoman newspaper. Caption: "Oklahoma senator David Boren, left, host a brunch for senators Robert Byrd of West Virginia and Lloyd Bentsen of Texas in the TransAmerica building Monday in San Francisco."

Photograph used for a story in the Daily Oklahoman newspaper. Caption: "Mark Russell, test manager for Forte Data Systems of Santa Clara, Calif., examines a communications board for personal computers."

Photograph used for a newspaper owned by the Oklahoma Publishing Company. Caption: "Mr. and Mrs. Kim Defenderfer / Bride and Groom."

Photograph used for a story in the Daily Oklahoman newspaper. Caption: "Dorian Harewood and Debbi Morgan star as Jesse Owens and his wife Ruth."

Photograph used for a story in the Daily Oklahoman newspaper. Caption: "The Jesse Owens Story, Dorian Harewood stars as Olympic track hero Jesse Owens in a paramount Television Domestic Distribution/Harve Bennett Productions major television event, "The Jesse Owens Story"

Photograph used for a newspaper owned by the Oklahoma Publishing Company. Caption: "Betty Hall, left, and Shirley Darrell, right, tabulate the Oklahoma delegation's vote on the minority platform proposal Tuesday at the DNC."

Photograph used for a newspaper owned by the Oklahoma Publishing Company. Caption: "Shirley Darrell, Oklahoma County Commissioner, was elected co-chairman of the Oklahoma delegation Monday."

Photograph used for a newspaper owned by the Oklahoma Publishing Company.

Photograph used for a story in the Daily Oklahoman newspaper.

Photograph used for a newspaper owned by the Oklahoma Publishing Company.

Photograph used for a newspaper owned by the Oklahoma Publishing Company.

Photograph of nine WASP members posed in two rows at a reunion. Most of the group is wearing some shade of pink in their attire. A note seen on the back of the photo reads, "San Diego Reunion 1984".

Clipping of a magazine article about WWII WASP serving as role models for female pilots in the U.S. Air Force. The article includes photographs of some of the WASP pilots.

Notice with information about the 1984 WASP Reunion, including date, time, location, room reservation procedure, and schedule of events.

Flyer for the WASP 1984 Reunion event, including a map of the hotel, details for registration and reservations, a schedule of events, and a tear-off form for registration. There is more information about the reunion on the back of the flyer.

Agenda for a general business meeting, concerning WASP matters.

Letter from Freda M. Breise to an Avenger Field Instructor discussing an upcoming WASP reunion in San Diego, from September 12, 1984 through September 16, 1984. The letter also includes a registration update with a tear-off form registration form.

Schedule for the 1984 WASP reunion celebration in San Diego, California, held at the Vacation Village Resort. The schedule includes addresses for the resort and registration, details for room reservation, information on optional activities, and the itinerary.

A survey of measuring devices or probes, which have been used to investigate gas-side fouling, has been carried out. Five different types of measuring devices are identified and discussed including: heat flux meters, mass accumulation probes, optical devices, deposition probes, and acid condensation probes. A total of 32 different probes are described in detail and summarized in matrix or tabular form. The important considerations of combustion gas characterization and deposit analysis are also given a significant amount of attention. The results of this study show that considerable work has been done in the development of gas-side fouling probes. However, it is clear that the design, construction, and testing of a durable versatile probe - capable of monitoring on-line fouling resistances - remains a formidable task.

Payload increases of three to five times that of the Shuttle/Centaur can be achieved using nuclear electric propulsion. Various nuclear power plant options being pursued by the SP-100 Program are described. These concepts can grow from 100 kW/sub e/ to 1MW/sub e/ output. Spacecraft design aspects are addressed, including thermal interactions, plume interactions, and radiation fluences. A baseline configuration is described accounting for these issues. Safety aspects of starting the OTV transfer from an altitude of 300 km indicate no significant additional risk to the biosphere.

The Advanced Servomanipulator (ASM) slave was designed with an anthropomorphic stance, gear/torque tube power drives, and modular construction. These features resulted in increased inertia, friction, and backlash relative to tape-driven manipulators. Studies were performed which addressed the human factors design and performance trade-offs associated with the corresponding master controller best suited for the ASM. The results of these studies, as well as the conceptual design of the dual arm master controller, are presented. 6 references, 3 figures.

SP-100 is the designation for a nuclear reactor-based power plant being developed for both civil and military missions beginning in the 1990s for such potential space applications as communication satellites, space radar, electric propulsion and space stations. Typically, a system using the SP-100 along with a selected upper stage system would be launched by the National Space Transportation System (NSTS) Space Shuttle System into a near-earth orbit, deployed, and through upper stage propulsion burn(s) be inserted/transferred to its mission orbit. The nature of the advanced design SP-100 gives rise to a set of issues that require special attention to assure that payloads using this power plant are physically and functionally compatible with the NSTS and meet the safety requirements thereof. The purpose of this document is to define and present the requirements and interface provisions that, when satisfied, will ensure technical compability between SP-100 systems and the NSTS.

This report delineates the scope of Jet Propulsion Laboratory`s FY`83 effort in the attitude control area in support of the SP-100 program. Dynamic modeling of the baseline beam configuration has been conducted and is presented herein. As a first cut, the beam is treated as rigid. Its inherent flexibility is then integrated via the hybrid coordinates method. Using the resulting dynamical equations, a preliminary look at attitude control is taken. Only one axis of rotational one flexible mode are included. An alternative to the beam configuration is one that envisions connecting basebody to user via a long, lightweight, flexible tether. A literature search has been conducted in this area and the resulting bibliography is presented. The tether option is not considered viable near term. However, it offers several potentially significant advantages and thus deserves serious consideration for the next generation space power system. This report also treats attitude control constraints imposed by the high temperature and radiation environment and addresses the issue of hardware requirements and availability. Recommendations for FY`84 tasks include assembling and exercising a simulation program for the beam configuration dynamic model and conducting a technology assessment in the area of tether dynamics and control.