User:Rlandmann/Specs proposal 2

Non-metric version of suggested specs section:

Specifications (variant described)
key to units

General characteristics

 * Crew:
 * Capacity:
 * Length: ft ( m)
 * Wingspan: ft ( m) or
 * Main rotor diameter: ft ( m)
 * Height: ft ( m)
 * Wing area: ft&sup2; ( m&sup2;) or
 * Main rotor area: ft&sup2; ( m&sup2;)
 * Empty weight: lb ( m)
 * Maximum gross takeoff weight: lb ( kg)
 * Powerplant: Engine type(s), lbf ( kN, kgf) thrust (each) or
 * Powerplant: Engine type(s), hp ( kW, PS) (each)

Performance

 * Maximum speed: (Mach) mph ( kt, km/h)
 * Cruise speed: mph ( kt, km/h)
 * Maximum range: mi ( nm, km)
 * Service ceiling: ft ( m)
 * Maximum rate of climb: ft/min ( m/min)
 * Maximum wing loading: lb/ft&sup2; ( kg/m&sup2;) or
 * Maximum main rotor loading: lb/ft&sup2; ( kg/m&sup2;)
 * Thrust/weight: or
 * Power loading: kg/kW ( lb/hp)

Armament

 * where applicable