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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 19 records

Thick ceramic coating development for industrial gas turbines - A program plan

A program plan on a NASA-Lewis funded program is presented, in which effectiveness of thick ceramic coatings in preventing hot corrosion and in providing thermal insulation to gas turbine engine components are to be investigated. Preliminary analysis of the benefit of the thermal insulating effect of this coating on decreasing cooling air and simplifying component design appears very encouraging. The program is in the preliminary stages of obtaining starting materials and establishing procedures. Numerous graphs, tables and photographs are included.

Vogan, J. W.

The Space Tug mission role and program planning.

More than half of the planned payload programs require a velocity increment beyond that nominally provided by the Space Shuttle. The reusable Space Tug system can satisfy this placement requirement and, in addition, can provide other, vital operational services for payloads in the 1980s. To realize maximum operational and economic benefits, it is desired that an orbital propulsive stage such as the Space Tug be available concurrently with Space Shuttle initial operations. Potential tug missions, significant interfaces, system characteristics, and configuration alternatives are discussed in conjunction with salient program planning factors.

Schnyer, A. D.

Manned Orbital Transfer Vehicle (MOTV). Volume 6: Five year program plan

The five year program plan for the manned orbit transfer vehicle (MOTV) is presented. The planning, schedules, cost estimates, and supporting data (objectives, constraints, assumptions, etc.) associated with the development of the MOTV are discussed. The plan, in addition to the above material, identifies the supporting research and technology required to resolve issues critical to MOTV development.

Boyland, R. E.