Societe Nationale des Constructions Aeronautiques du Sud-Ouest (SNCASO) - France
Ability to conduct aerial bombing of ground targets by way of (but not limited to) guns, bombs, missiles, rockets, and the like.
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
Maximum Take-Off Weight
2 x Rolls-Royce Nene 102 turbojet engines developing 5,000lb of thrust each.
(850 kph | 459 knots)
MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
2 x 15mm MG151 autocannons in port side, rear-facing gun barbette wingtip pod.
2 x 15mm MG151 autocannons in starboard side, rear-facing gun barbette wingtip pod.
Up to 11,000lb of internally-held stores in the form of conventional drop bombs.
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 (528mph).
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).