McDonnell Douglas - USA / Hawker Siddeley - UK
United Kingdom (planned, cancelled); United States (planned, cancelled)
(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the McDonnell Douglas AV-16A production variant)
1 x Rolls-Royce Pegasus 15 non-afterburning turbofan engine developing an estimated 24,500lb of thrust for lift and propulsion.
(1,160 kph | 626 kts)
(15,000 m | 9 mi)
(3,300 km | 6,112 nm)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
STANDARD, FIXED (Royal Air Force):
1 x 30mm ADEN internal automatic cannon.
STANDARD, FIXED (USMC):
1 x 25mm GAU-12 internal automatic cannon (5-barreled Gatling-type).
OPTIONAL (RAF and USMC):
Up to seven external hardpoints (three to each wing) for the carrying of air-to-air and air-to-surface missiles as well as precision-guided bombs, conventional drop bombs, rocket pods, and jettisonable fuel tanks.
(Not all ordnance types may be represented in the showcase above)
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.