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MIL-T-18232B(AS)
3.1.3.3
WEIGHT EMPTY
AERO. SURFACE GROUP
Wing
Fin
Stabilizer
BODY GROUP
TAKEOFF AND RECOVERY GROUP
PROPULSION GROUP
Liquid system
Solid System
Air Breathing System
Nuclear System
Fuel and Lub System
Oxidizer and Lub System
POWER GENERATING GROUP
Prime Power source
Hydraulic and Pneumatic
Electrical
ORIENTATION CONTROL GROUP
Aerodynamic
Thrust and Reaction
GUIDANCE GROUP
ELECTRONIC GROUP
ENVIRONMENTAL PROTECTION GROUP
Temp. Cont. - Struct.
- Equip.
Compressed Press. System
Ground Service Prov.
ARMAMENT GROUP
MISCELLANEOUS
step Separation system
Destruct System
Emergency Equipment
Visual Identification
3.1.4
CENTER OF GRAVITY LOCATION. - Center of gravity, launching
and normal flight conditions for gross weight, empty weight
and external stores and full payload condition.
Normal Flight
Launching
General and Air Launch
Condition
Condition
Horizontal (inches  from datum) or
(%M.A.C. aft of L.E.M.A.C.)
Vertical (inches (above)(below) waterline or centerline reference)
7

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