SPACE TUG THERMAL CONTROL Summary Report, 1 Jul. 1973-30 Apr 1974

摘要

A series of three catalogues were created to provide representa-tive equipment data for use in the study. The catalogues were particularly useful in the study and rather unusual at this point in the development of a spacecraft. Additional information could be added to the catalogues to further expand the usefulness of this approach.nSignificant thermal control systems were carried an additional step to include a preliminary set of design and performance spec¬ifications. Three specifications were developed covering specific areas of concern relative to the forward compartment thermal de¬sign, battery louvers, and fuel cell heat rejection system.nA follow-on plan was developed highlighting the breadboard testing of the above key areas, which were advanced to the preliminary specification phase including a honeycomb conductivity test. In addition, several areas of analytical concern were identified that were beyond the original scope of the study.