Template:Prelaunch checklist

When it's possible, the original Apollo documentation is used for the checklists. Steps, which are not possible at the moment, are denoted in grey. Additionally there are checklists in Word file format in the Doc\Project Apollo - NASSP\Check List directory of your installation. Procedural steps in this section are presented in tabular form and in sequence they occure during the mission. The following is a detailed explanation of the columnar data presented in the tabulated lists:

Apollo 15 launch checklistA15_LAUNCH_CHECK

Time	This column contains the mission time the procedure is to be done. Sometimes there's no fixed time when to do a procedure, in that case the time is left out.
Procedure	The procedure is a group of steps or overall tasks involved in performing a complete function or operation. It often consists of controls the astronauts have to toggle or display readings that have to be checked. See CSM panels for more informations.
Panel	The panel number of a particular switch or display for easier panel navigation.
Remarks	Any useful comment. Please notice especially differences to the original function, bugs or other issues.

Spacecraft systems activation

In Project Apollo - NASSP the Saturn prelaunch checklist starts at 3 hours before launch with the backup crew in the spacecraft. At first some of the spacecraft's systems have to be activated.

Time	Procedure	Panel	Remarks
-03:00:00	C/W system activation     C/W POWER - 1 (up)   MASTER ALARM pb/lt (3) - on,   push	2	The suit compressor alarm is normal.
	CMC power up   cb G/N COMPUTER MNA - close cb G/N COMPUTER MNB - close	5	Activation of the command module computer.

{{ #if: |

V37E 00E   P00   If prog alarm, check if alarm code 1520 "V37 request not permitted at this time" by V05N09E, then RSET and retry V37E 00E   V35E   F 88 88 V37E 00E   V16 N65E   16 65 V37E 00E

2

Run program P00 This can happen every V37 request. Light test Shows time since power-up, check time synchronization with Orbiter.

|

Wait until DSKY light test complete   STBY lt - on PRO   STBY lt - out Key N00E   P00   NO ATT lt - on Key V34E Key V16 N33E

2

Light test isn't historically correct. Run program 0, the AGC idling program. IMU is not turned on. Show launch countdown (not historically correct).

}}

IMU power up   cb G/N IMU HTR MNA - close cb G/N IMU HTR MNB - close cb G/N IMU MNA - close cb G/N IMU MNB - close     {{ #if: |NO ATT lt - on (90 sec) |NO ATT lt - off }}   {{ #if: |NO ATT lt - off | }}

5         2

Activation of the inertial measurement unit.

Backup crew prelaunch checks

C&WS status check

With the first procedure the caution and warning system is checkedAOH2.

Glycol loop checks

Next the primary and secondary water-glycol coolant loops are checked and the primary water-glycol coolant loop is activated. The grey lines indicate displays or controls which are not available at the moment, please ignore these steps.

Standby inverter checks

Time	Procedure	Panel	Remarks
	C/W NORM - BOOST	2	This is not mentioned in the Apollo Operations HandbookAOH2, but otherwise the C/W lights during the inverter check won't work.

Panels checks

Next some checks regarding the panel displays and controls have to be done and a few but very important devices have to be turned on. We begin at panel 325, which is to the left of the left side panel.

Time	Procedure	Panel	Remarks
	PRIM GLY TO RAD vlv - NORM	325
	AUTO RCS (16) - OFF SECS LOGIC (both) - OFF SECS PYRO ARM (2) - SAFE cb pnl 8 - all closed except   cb CM RCS HTRS (both) - open   cb FLOAT BAGS (all) - open   cb SECS LOGIC (2) - open   cb SECS ARM (2) - open	8
	EDS PWR - OFF TVC SERVO PWR (both) - OFF FDAI/GPI POWER - BOTH LOGIC 2/3 PWR - on (up) ELEC PWR - GDC/ECA SIG CONDR/DR BIAS PWR (both) - AC1 or AC2 BMAG PWR (both) - WARMUP	7	Turn on both FDAIs. Turn on GDC and ECA. Powers RJ/EC. Switches should not be set on same bus.
	CMC ATT - IMU ACCEL - check (+1 G) FDAI SCALE - 5/1 FDAI SEL - 1/2 FDAI SOURCE - CMC ATT SET - GDC MAN ATT ROLL - RATE CMD MAN ATT PITCH - ACCEL CMD MAN ATT YAW - RATE CMD LIM CYCLE - OFF ATT DBD - MIN RATE - HI THC PWR - on (up) RHC PWR NORM (both) - AC/DC RHC PWR DIR (both) - OFF   SC CONT - SCS CMC MODE - FREE BMAG MODE (3) - RATE 2 ATT SET TW (3) - R 162°, P 90°, Y 0°   ELS LOGIC - OFF ELS AUTO - AUTO CM RCS LOGIC - OFF CM PRPLNT DUMP - OFF CM PRPLNT PURG - off (down) IMU CAGE - off (down)   α/Pc IND sw - α α/Pc ind - zero LV IND/GPI sw - GPI EVNT TMR START - ctr EVNT TMR RSET - up (ctr)	1	Activate Trans. Contr. Pwr. Activate Rot. Contr. Pwr. These are the nominal values for a 72° launch azimuth. Guarded. Guarded. Guarded. Guarded. Switch to α. Event timer not counting. Timer resets and starts automatically when lift-off occurs.
	SUIT CAB ΔP ind - > + 2.0 inH2O O2 FLOW ind - 0.4 ± 0.1 lb/hr   PROBE EXTD/REL tb (2) - gray PROBE (3) - OFF   RCS status check   SM RCS He 1 tb (4) - bp   SM RCS He 2 tb (4) - bp   SM RCS PRIM PRPLNT tb (4) - bp   SM RCS SEC PRPLNT tb (4) - bp   EDS AUTO - OFF CSM/LM FNL SEP (both) - off (down) CM/SM SEP (2) - off (down) SIVB/LM SEP - off (down) PRPLNT DUMP - AUTO 2 ENG OUT sw - AUTO LV RATES sw - AUTO TWR JETT (both) - AUTO LV GUID sw - IU LV STAGE - OFF XLUNAR INJECT - INJECT MN REL - off (down)	2	Gray indicates probe fully extended or retracted. Barber pole indicates valves are closed. Guarded. Guarded. Guarded. Guarded. Guarded. Guarded. Guarded.
	FC 1 PUMPS - AC1 FC 2 & 3 PUMPS - AC2 MN BUS TIE (2) - OFF BAT CHGR - AC1 cb pnl 5 - all closed	5
	GLY PUMPS - 1 AC1 SUIT COMPR (both) - OFF cb pnl 4 - all closed	4

Test

{{ #if: |Virtual AGC |NASSP AGC }}

Test End

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1. References

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