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

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SUIT PGA PRESSURE INDICATOR (LEFT FOREARM) 5M2A-03-SC01 2 APOLLO OPERATIONS HANDBOOK PERFORMANCE TEMP I [_ PREss-------] CABIN SUIT CABIN PARTPRESS CO2 NOTES:. I A vertical green color bond shows the normal operating range for the suit temperature (45 ° to 65°F). Red horizontal i;nes show limits for suit pressure (3.4 ps;o), cabin pressure (4.7 ps;o), and CO2 pressure (|5 mm Hg). A vertical yellow color Ixmd shows the caution range for CO 2 pressure(7.6 to 15 mm Hg). 2..The PGA pressure indicator presents an operating rOfige frcxn 2 to 10 psio and a green and red color b_nd. The green I:_nd (3.5 to 10 psio) shows normal pressure requlreddurln 9 space flight. The redb_nd(3.Sto 2pslo) shows the emergency limitations for crave safety. During ground operations, the indicator needle will be.pegged beyond 10 psio because of atmospheric pressure. Figure ..-;. ECS Suit. and. Cabin Temperature/Pressure Indicators S-BAND ANT Auxiliary DC VOI T_ Me , S-BAND ANT Meter i 77Y',: "T:'FLA'," SM- 2A - 697C SM-2A-693C _T le ] ] 1 I i! t I J 1 I I I I I I ] -p
i i i I I i I I I I I i I I I , 4.1.5.2 ' 16 4..o.L SMZA-03-SC01 2 APOLLO OPERATIONS HANDBOOK PERFOP$_ANCE switches to monitor 13 EPS, 6 RCS, 4 G&N and 1 ECS analog measurements. Refer to Controls and Displays (section 3) for information on which measurements are selected for monitoring by the auxiliary DC VOLTS meter. The voltmeter provides a reading between 0 and 5 volts of the selected measurement. By use of a voltmeter conversion chart an interpolation of the value for the selected measurement can be made. (Refer to section D.) NOTE The accuracy of the auxiliary DC VOLTS meter (.for the full scale) is zl percent at 75°F.and ±2 percent at 0 ° and 150°F. S-Band ANT Meter. The S-Band ANT meter, on NDC-19 (figure 4-i0), utilizes the automatic gain control (AGC) signal in the S-Band receiver to display, in a clockwise direction, the relative magnitude of signals received by the unified S-band equipment (USBE). The meter is used in determining the correct S-band antenna and S/C attitude for optimum S-band performance. NOTE The accuracy of the S-BAND ANT meter (for the full scale) is z5 percent at temperatur@s between OOand 150°F. SEQUENTIAL SYSTY_JS INDICATORS. Instrument markings for the sequential systems indicators are sho_m in figur2 4-L[. The indicators present visual dfsplays required during launch, in-flight SPS operation, and the earth landing sequence of evenis. (Refer to paragraphs !,.1.6.l and 4.i.6._.) Barometric Pressure Indicator (Altimeter). The barometric pressure indicator, an altimeter on _C-i (figure 4-_Z), is used in conjunction with the earth landing system (ELS) and indicates the pressure altitude of the S/C under low-altitude, low-Mach conditions. This altimeter is monitored during the earth landing phase of the mission to verify that the ELS sequencer is initiating various phases of landing system deployment at the _ro_cr _ressure altitude points. A knob, located left of the altimeter qial face, is used in setting the adjacent marker.(to display the corrected main parachute deploy altitude for low-altitulc aborts). The adjustable marker, based
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Apollo 204 Review Board Appendix C Section 2 - NASA's History ...

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