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Mckhann, G. G.

Publications and source records attributed to Mckhann, G. G..

5 records
All sourcesNASA NTRSDOE OSTI
NASA NTRS1978

Photovoltaic power-system options for the manned space construction base

The function of the proposed manned Space Construction Base (SCB) is to provide a permanent manned orbital facility for the construction and operation of a variety of space experiments, ranging from a space-processing development to on-orbit-constructed microwave radiometers and antennas. A typical SCB system might reach initial operational capability in low earth orbit in 1985, have a 10-year mission duration, and have an initial power requirement of 50 kWe. A summary of the requirements imposed by the SCB on the electrical power system (EPS) is presented in a table. Attention is given to EPS options, baseline power platform system operations, an energy storage system evaluation, advanced-technology NiCd batteries and lifetime, and orbital buildup operations.

Mckhann, G. G.↗
NASA NTRS1977

Space construction base operations in support of solar power satellite development

Development of the Solar Power Satellite (SPS) system for initial operation in the late 1990's requires substantial orbital development activities in the mid-1980's leading to a key system development decision in about 1987. A manned Space Construction Base (SCB) in low-earth orbit is needed to support the SPS orbital development program. The SPS system development issues are defined, along with a candidate development program for resolving these issues. The development hardware systems of interest for the mid-1980's include: (1) a tapered linear array microwave antenna (123 x 125.6 m 'cross') with a 57-kW/rf amplitron output, which is SCB constructed and operated in low-earth orbit initially, and, subsequently, unmanned in geosynchronous earth orbit; and (2) a SCB-constructed and -operated 9 x 14.4 m planar array antenna (358 kW/rf/) powered by a 455-kWe silicon photovoltaic solar collector.

Mckhann, G. G.↗
NASA NTRS1972

Preliminary design of reactor power systems for the manned space base.

The results of design integration studies of uranium-zirconium hydride (UZr-Hx) reactor power systems for the NASA space base study program are presented. The power conversion systems investigated include the Brayton cycle, the organic Rankine cycle, the SNAP-8 mercury Rankine cycle, and thermoelectric (PbTe). The proposed space base has a 10-year life and requires 100 kWe of power. Two 50-kWe power systems with a nominal replacement life of 5 years are utilized. Parametric design data such as life, weight, radiator area, reactor outlet-temperature, reactor thermal power, and power conversion system efficiency are presented and used for the design and integration of the system with the space base.

Mckhann, G. G.↗