Drake TR-270 FM Transciever

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The improved parasol w a s c a r r i e d by t h e second crew. Major resupply items f o r t h e second manned period were t h e supplementary r a t e gyro package and cables, the improved parasol, experiment f ih, f m d f o r a 3-day mission extension, various assemblies t o replace f a i l e d experiment components, and two laboratory d a t a tape recorders. 65 psia. Xepressurization began imnediately and w a s terminated a t 5 psia approximately 20 boilrs before launch. h sequence of major events of the second unmanned period is shown i n f i g u r e 3-15.

The program was used on a d a i l y b a s i s during the mission, p a r t i c u l a r l y i n t h e a n a l y s i s of proposed Z l o c a l v e r t i c a l and quasii n e r t i a l a t t i t u d e modes. It was a l s o used on an around-the-clock b a s i s during the c r i t i c a l period following t h e launch of the Saturn Workshop. The program proved t o be extremely valuable i n mission p r o f i l e a n a l y s i s and power management. The power system simulator located a t Marshall consisted of flight-type power equipment except f o r s o l a r arrays, which were simulated.

1 Activation S h o r t l y a f t e r o r b i t a l i n s e r t i o n , t h e P i l o t began t o experience motion s i c k ness. H e obtained r e l i e f by taking one anti-motion-sickness capsule and w a s a b l e t o p a r t i c i p a t e i n t h e a c t i v a t i o n a f t e r docking. Rendezvous w a s s u c c e s s f u l l y attained and a flyaround i n s p e c t i o n a s performed. During t h e flyaround the spacec r a f t w c s flown s o near t h e thermal p a r a s o l t h a t t h r u s t e r exhaust impingement caused movement t h r e a t e n i n g p a r a s o l damage.

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