The following conditions should be observed after propellant tanks are pressurized with APUs in operation, but before the engine is fired:
System Monitor Panel
- Ammonia tanks – Internal tanks, 1445 gallons; external tanks 1053 gallons (approx.).
- Liquid oxygen tanks – Internal tanks, 1017 gallons; external tanks, 770 gallons (approx.).
- Turbopump hydrogen peroxide (H2O2) tanks – 118 gallons.
- Solid fuel (X-15AD-4 airplane only) – Both boosters, 100 percent.
- Propellant source (helium) tanks – Both internal and external tanks, 3200-3800 psi.
- Engine and propellant control source (helium) tanks – Both internal and external tanks, 3200-3800 psi.
- Auxiliary pneumatic and control (helium) tank – 3200-3800 psi.
- APU H2O2 tanks – 60-75 gallons, both pointers, gradually decreasing.
- APU source (helium) tanks – 3200-3800 psi, both pointers, gradually decreasing.
- Liquid N2 tank – 25-30 gallons, gradually decreasing.
- Cabin helium tank – 3200-3800 psi, gradually decreasing.
- Pilot's O2 (seat) cylinders – 3000-3200 psi.
Main Instrument Panel
- Propellant source pressure gauge [69, fig. 5-1] – Both internal and external tanks, 3200-3800 psi.
- H2O2 source pressure gauge [57, fig. 5-1] – Both internal and external tanks, 3200-3800 psi.
- Propellant tank pressure gauge [71, fig. 5-1] – 45 to 53 psi (both pointers).
- External tanks fuel flow indicator [4, fig. 5-1] – 50%.
- Propellant pump inlet pressure gauge [72, fig. 5-1] – “L” pointer, 40 to 70 psi; “A” pointer, 40 to 55 psi.
- APU source pressure gauge [45, fig. 5-1] – 3200-3800 psi, both pointers, gradually decreasing.
- APU H2O2 tank pressure gauge [44, fig. 5-1] – 550 to 610 psi (both pointers), gradually decreasing.
- Cabin helium source pressure gauge [40, fig. 5-1] – 1000 to 3400 psi.
- Hydraulic pressure gauge [13, fig. 5-1] – 2900 to 3400 psi (both pointers).
- Mixing chamber temperature gauge [42, fig. 5-1] – -45° C to -35° C (both pointers).
- Generator (AC) voltmeter [22, fig. 5-1] – 195 to 205 volts, both pointers (internal power if generators are ON).
- APU bearing temperature gauge [43, fig. 5-1] – 80° C to 130° C (both pointers), gradually increasing.
- H2O2 tank and engine control pressure gauge [55, fig. 5-1] – “T” pointer, 0 psi; “C” pointer, 575-600 psi.