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THE JOHNS HOPKINS UNIVERSITY

APPLIED PHYSICS LABORATORY

LAUREL MARYLAND

APPENDIX A

All of the figures in Appendix A are taken from Section 4 of "Interim Summary Report Investigation of a 15 KW Solar Dynamic Power System for Space Application," which is available in its entirety from The Defense Documentation Control Center under AD 432202. These figures reflect the previously developed state-of-the-art in "Space Deployable" solar concentrating mirrors. They are arranged in their original order. Note that the reradiation versus absorber size dilemma is specifically recognized in the original text under Figure IV.2-20. Note also that some of the figures are of poor quality in the original microfilm from which they have been reproduced. They are reproduced for the reader's convenience due to the current unavailability of hard copies.

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FOAM GENERATOR

I

A-5

ENTRATOR DEPLOYMENT
SECOND STAGE

Foam Generation, Placement

And Curing

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