Apollo 204 Review Board Appendix C Section 2 - NASA's History ...

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.. l ( L i ! I I 1 ) i I I i Mission SMZA-03-SC01Z APOLLO OPEI_ATIONS HANDBOOK EXPERIMENTS AND SCIENTIFIC EQUIPMENT DATA SECTION 5 EXPERIMENTS AND SCIENTIFIC EQUIPMENT DATA INTRODUCTION This section presents the objectives of mission Z04A experiments and Contains a description of associated equipment, stowage areas (figure 5-I), crew participation requirements for data collection, and related scientific equipment data. The in-flight tests are categorized as medical (M-), scientific (S-), and technical (T-) experiments as follows: • In-Flight Exerciser (M-3A) (M003) • In-Flight Phonocardiogram (M-4A) (M004) • Bone Demineralization (M-6A) (M006) • Human Otolith Function (Vestibular Effects)(_Vi-9A) (M009) • Cytogenetic Blood Studies (M-II) (M011) • Cardiovascular Reflex Conditioning (M-48) (M048) • Synoptic Terrain Photography (S-bA) (S005) • Synoptic Weather Photography (S-6A) (S006) • In-Flight Nephelometer (T-3) (T003). NOT_ The planning and Management Office of the EPO (Experiments Program Office) is the coordinating facil- ity for all of the experiments described in this section. The experiments sto_.vage areas location will be found in {igure 5-i. SCIENTIFIC EQUIPMENT.. MEDICAL DATA ACQUISITIO -_: SYSTEM (MDAS). The medical data acquisition system, located in compartment C (figure 5-Z), weighs 15.Z pounds and consists of a seven.channel tape recorder, associated signal conditioners, junction box, time code generator, and a front panel with switches and outlets for power and signal cables. This GFE unit uses Z8-volt d-c power from compartment A to acquire and permanently record on magnetic tape all required medical (operational and. experimental) data. The operational data.required consists of electro- cardiograph and impedance pneumograph outputs, while the experimental data consists onlyo{ phonocardiograph,outputs. These medical parameters are routed from sensors and signal conditioners (attached to a crewman) through the PGA or CWG adapter cable, cobra cable, T-adapter, and octopus cable to specified channels in the MDAS. Although I00 watts of 'ectrical power is provided for the MDAS from compartment A via the :topus cable, only about 19 watts are needed to operate the integraltape "" i i- - 7r ..... i -- irl- ] 1 [ I SCIENTIFIC EQUIPMENT _ __.,, Basic Date 12 Nov - - 1.966 i " -Chan_e Date -, Page _-I
Mission SM_A-03-SC012 APOLLO OPERATIONS HANDBOOK EXPERIMENTS AND SCIENTIFIC EQUIPMENT DATA SCIENTIFIC EQUIPME NT Basic DaCe ..l.Z_Nqv_!966 ChanRe Dale -
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Apollo 204 Review Board Appendix C Section 2 - NASA's History ...

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