A brief narrative outline is presented of a scenario for the development of the Atlantic Coastal Plain hydrothermal resources for geothermal space heating and cooling. Listed below are the basic assumptions made in the construction of this scenario. Since this scenario is to serve as a planning document, the steps involved in geothermal development are listed and time-phased. The most critical steps in this process are indicated. This scenario summarizes geothermal development in the entire Atlantic Coastal Plain. Separate, more detailed scenarios for each specific resource area are planned as precursors to possible implementation planning.

A brief narrative outline is given of a scenario for the development of geothermal heating and cooling, (1) in the Hot Springs, Little Rock, and Pine Bluff area of central Arkansas, and (2) in the southern Arkansas area. Basic assumptions about details of the scenario and the data included therein are listed. The scenario in chart form is included. (MHR)

An economic feasibility study for a geothermal community heating system has been made for the residential heat load of Cape Charles, Virginia using the JHU/APL GRITS Computer Program. The effects of inflation, interest rates, wellhead temperatures, and the addition of reinjection wells are investigated.

Reentry analyses consisting of ablation response, thermal response and thermal stress response have been conducted on the Light Weight Radioisotope Heater Unit for Galileo/VEEGA reentry conditions. Sequential ablation analyses of the LWRHU aeroshell, the fuel clad, and the fuel pellet have been conducted in reentry regimes where the aeroshell has been deemed to fail. The failure criterion for ablation is assumed to be recession corresponding to 50% of the wall thickness (the design criterion recommended in the DOE Overall Safety Manual). Although the analyses have been carried far beyond this limit (as presented and discussed herein), JHU/APL endorses the position that failure may occur at the time that this recession is achieved or at lower altitudes within the heat pulse considering the uncertainties in the aerodynamic, thermodynamic, and thermo-structural analyses and modeling. These uncertainties result mainly because of the high energies involved in the VEEGA reentries compared to orbital decay reentries. Risk evaluations should consider the fact that for shallow flight paths the unit may disassemble at high-altitude as a result of ablation or may remain intact until it impacts with a clad that had been molten. 80 refs., 46 figs., 16 tabs.