(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the base Breguet Br.1100 production variant)
2 x Turbomeca "Gabizo" afterburning turbojet engine developing 2,670lb of dry thrust and 3,310lb of thrust with reheat.
(1,130 kph | 610 kts)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
(Showcased performance specifications pertain to the base Breguet Br.1100 production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
PROPOSED (FIXED, FORWARD-FIRING):
2 x 30mm DEFA 551 autocannons.
1 x MATRA retractable rocket battery launcher in belly.
Up to two hardpoints supporting aerial rockets, gun pods, rocket pods, and conventional drop bombs as needed.
(Not all ordnance types may be represented in the showcase above)
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
The overall rating takes into account over 60 individual factors related to this aircraft entry.
Rating is out of a possible 100 points.
This entry's maximum listed speed (702mph).
Graph average of 563 miles-per-hour.
Showcasing era cross-over of this aircraft design.
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.