I will make a SNCASE & Sud-Aviation list;
SE-161 Languedoc was a forty-seat transport monoplane,started as the Bloch MB-161
SE-20 Aquilon was a license-built De Havilland Sea Venom
SE-201 Aquilon was a two-seat night pursuit version of 1952
SE-202 Aquilon was a DH Sea Venom derivative
SE-203 Aquilon was a single seat fighter version
SE-204 Aquilon was a two-seat jet trainer version
SE-247 was developed from LeO H-47,as a military derivative version of 1945
SE-520 was a Projected version of Dewoitine D.520
SE-520Z was ex Dewoitine
SE-530 Mistral was a license-built De Havilland Vampire
SE-531 Mistral was a license-built De Havilland Vampire with Nene 102B engine
SE-532 Mistral was a license-built De Havilland Vampire with Nene 104 engine and ejector seat
SE-533 & SE-534 Mistral were unknown variants,maybe a Projects
SE-535 Mistral was a navel fighter version
SE-580 was a post-war Project fighter derived from D.520 with dorsal air intake,powered by one Hispano-Suiza 12Z
engine
SE-581 was a Project version,powered by one 2500 hp Hispano-Suiza 24Z engine
SE-582 was a Project version,powered by one 4000 hp Arsenal 24H engine
SE-100 was an initially designed the LeO 50,powered by two 1081 hp Gnome-Rhône 14N-20 or Gnome-Rhône 14N
-21 engines
SE-100-02 was a version of SE-100,powered by two Gnome-Rhône 14N
SE-101 was a three-seat fighter in C.3 category,powered by two 750 hp Hispano-Suiza 14 AB-02/03 engines,later
re-engine with 1100 hp Pratt and Whitney Twin Wasp R-2000 engines
SE-102 was a three seat observation light bomber version,in AB3 category,powered by two Gnôme-Rhône 14 N2/3
or 14N40/41 engines
SE-103 was anther AB3 version,powered by two 1150 hp Hispano-Suiza 14AA-12/13 engines
SE-104 was unknown version
SE-105 was a version of SE-100,with two auxiliary tanks and powered by two 1320 hp Gnôme-Rhône 14 R4/5 engines
SE-110 was an initial name for SE-101
SE-120 & SE-121 maybe were a single seat mono-motor fighter Projects,need confirm
SE-122 was a single seat recce Project version of SE-100,a scale down configuration,powered by single engine,driven
two counter-rotating propellers
SE-200 Amphitrite was a formerly LeO H-49 large transport flying boat,powered by six 1600 hp Gnome-Rhône 14
R-26 & R-27 engines
SE-200 Lourd was a very heavy Project version,with 200 ton empty weight
SE-200 Affine was a version,with single-tail empennage and elongated hull,powered by six Gnôme-Rhône 18R and
78 ton empty weight
SE-200/4 was a four engined Project version,and simplified configuration
SE-201 & SE-202 were unknown variants,maybe a Projects only
SE-203 was a version,powered by six Gnome-Rhône 14R engines,and 68 ton empty weight
SE-204 was a version,powered by six Gnôme-Rhône 18R engines,and 80 ton empty weight
SE-204M was a military version of SE-204,powered by six Gnôme-Rhône 18R engines,with defensive and offensive weapons
SE-205 & SE-206 were unknown Project versions
SE-207 maybe was aversion ,powered by six Gnôme-Rhône 18R engines,and 90 ton empty weight
SE-208,SE-209,SE-210 & SE-211 were unknown Project versions
SE-212 was a Project version of SE-200,powered by six Gnôme-Rhône 18R, wing area increase of 35 m° and 90 ton empty weight
SE-300 was a light transport autogyro Project,powered by one 350 hp Gnôme-Rhône engine
SE-300T was a twi engined project for T3 category (ex Ronamo 111)
SE-400 was a three-seat mid-wing surveillance seaplane,on floats,powered by two 655 hp Gnôme-Rhône 14M
engines
SE-500 was a four seat light bomber Project version of SE-100,powered by two 1050 hp Gnôme-Rhône N-48/49
or 1600 hp Gnôme-Rhône 14R engines
SE-500T was a twin-engine 12 passenger cargo/transport Project,powered by two 1050 hp Gnôme-Rhône 14R
engines
SE-600 was a two-seat armed recce experimental Project,based on SE-100,but powered by one 350 hp Bearn
6D engine
SE-600/I was a light transport Project version,also powered by one 350 hp Bearn 6D engine
SE-700 was a three-seat passenger autogyro,powered by one 330 hp Béarn 6D-07 engine
SE-700S was an improved version,maybe remained a Project,
SE-701 was a version,intended to carry 700 kg of load,powered by one 220 hp Renault 6Q-01 engine,also known
as SE-700A
SE-702 was a version,featured by a fuselage hull and a fixed front wheel,powered by one 330 hp Béarn 6D-07 engine,
also called SE-700B
SE-800 was a transport Project developed from SE-100,22 passenger and four crew,powered by either 1350 hp
Gnome-Rhône 14 or 1650 hp Wright Cyclone engines
SE-800A was a 24 passenger and four crew,powered by two 1300 hp Gnome-Rhône 14 R engines,Project
SE-800B was a 33 passenger and four crew,powered by four 1000 hp Hispano-Suiza 12 Y engines,Project
SE-800C was a 24 passenger in cabin waterproof,powered by two 1600 hp Gnome-Rhône 14 R engines,Project
SE-900 was a high-wing twin engined flying boat project,may intended for military and civil roles
SE-1000 was a mid-wing stratospheric transatlantic postal transport monoplane Project,powered by four
1590 hp Gnome-Rhône 14 R engines
SE-1001 was a Project version of SE-1000,with re-designed the nose and cockpit configuration,as a long-
range mail carrier
SE-1010 was a high-altitude photo-survey aircraft,powered by four 1600 hp Gnome-Rhône 14 R-28/29 engines
SE-1011 was a production aircraft: three under construction when Project was abandoned
SE-1015 was a long-range 18 passenger courier airliner Project,powered by four 1600 hp Gnome-Rhône 14 R-28/29 engines
SE-1020 was a maritime patrol aircraft Project,with gun turret,powered by four Junkers Jumo 213 engines
SE-1030 was a proposed 40 passenger airliner variant Project,powered by four 1600 hp Gnome-Rhône 14 R-28/29 engines
SE-1035 was a high Speed Stratospheric airliners from 1947 with a more conventional larger diameter airliner
fuselage design,powered by four 1600 hp Gnome-Rhône 14 R-28/29 engines
SE-1040 was a proposed turboprop test-bed to evaluate the Rolls-Royce Dart engine
SE-1100 was a redesigning of SE-200C.,as a civil/military transport flying boat Project,120 ton empty weight
SE-1200 was a 125 passenger heavy version of SE-200,but powered by eight 3400 hp Arsenal 24H engines,
140 ton empty weight,Project
SE-1210 was a sub-scale version of SE-1200,powered by four 240 hp Renault 6Q engines
SE-1200/I was a medium transport compound helicopter Project,with shoulder wing and addition two
piston engines,mounted on it and the a low rear wing with twin tail fins
SE-1300 was a very large and heavy version of SE-200,with 180 ton empty weight,Project
SE-1400 was a projected sub-scale flying mock-up of SE 2400 or heavy jet fighter derived from SE 2400,powered
by one Rolls Royce Derwent V turbojet engine,Project
SE-1410 was a projected sub-scale flying mockup of SE 2400,but powered by Walter HWK 109/509 rocket
engine
SE-1400/I was a side-by-side two seat attack aircraft Project,powered by two Hispano-Suiza Nene turbojets,mounted
beside the fuselage with wing roots,later redesigned and developed into SE-2450
SE-1500 was a unguided, effect of explosions, 10 to 200 m from the vehicle (1946)
SE-1501 was a unguided target (1948)
SE-1502 was a unguided target (1950)
SE-1502M was a Navy recoverable target (1953)
SE-1503 was a turbojet powered target (1953)
SE-1504 was a developed project version of SE-1500
SE-1510 was a guided and recoverable target(1948)
SE-1511 was a test of optical guidance (1952)
SE-1520 was built but not flown; five were modified into SE 1502M and five more into SE 1523
SE-1521 was a experimental flying bomb (1949)
SE-1522 was a recoverable target (1952)
SE-1523 was a Navy operational recoverable target (1953)
SE-1524 was an Air Force operational recoverable target (1953)
SE-1530 was a built and not flown; seven were modified into SE 1522 and two into SE 1523.
SE-1531 was a rocket powered variant (1952)
SE-1600 was an experimental aircraft with additional vertical control surfaces Project,no more details
SE-1700 unknown Project,maybe a tourism glider,need confirm
SE-1800 was an two-seat experimental twin-jet transport flying wing Project,powered by two Rolls Royce Nene
turbojet engines
SE-1801 was a Project version of SE-1800,but powered by two Snecma ATAR turbojet engines
SE-1802 was a Project version of SE-1800,also powered by a less propulsion Rolls Royce Nene turbojet engines
SE-1900 was a rocket-powered wheeled car
SE-1910 was a record-breaking variant of above
SE-2000 was a mid-wing transatlantic heavy transport Project,powered by four 2100 hp Gnôme Rhôme R18
engines
SE-2001 was a unknown Project version,need Info
SE-2010 Armagnac was a enlarge version of SE-2000,with a cantilever mid-wing monoplane with retractable tricycle landing gear,powered by four 3500 hp Pratt & Whitney R-4360-B13 Wasp Major engines
SE-2020 was a version of SE-2010 with bigger wheels (1,72 m instead of 1,52 m),Project,maybe powered by
the same engines
SE-2030 was a version of SE-2010,but powered by four Cyclone turboprop engines
SE-2040 was a projected derivative of SE-2010,with four Allison T40 turboprop engines and longer fuselage
SE-2043 was a Project version from SE-2010,powered by four Bristol Proteus turboprop engines
SE-2050 was unknown Project version,need Info
SE-2060 was a test bed aircraft of SE-2010 transport aircraft with eight ATAR engines
SE-2100 was a two-seat light and touring tailless airplane,powered by one 190 hp Renault 4Pei pusher engine
SE-2200 was a single seat naval fighter Project,based on SE-580
SE-2300 was a two-three seat low-wing light and touring monoplane,powered by one 140 hp Renault 4Pei engine
SE-2301 was a developed version of SE-2300,need Info,maybe a Project
SE-2310 was a three-seat, tricycle undercarriage version,powered by one 190 hp Renault 4Pei engine
SE-2311 was a version of SE-2310,with retractable gear and fuel canisters in wings,maybe with the engine
SE-2320 was a project to a four-seater version of SE 2310 with 3-wheel retractable landing gear
SE-2400/I was a low-mid-wing single seat experimental attack monoplane Project,powered by two Socema CEM
turbojet engines,mounted under each wing
SE-2400/II was a single seat mid-wing experimental attack monoplane Project,powered by two Rolls Royce Nene
turbojet engines,mounted in dorsal intakes
SE-2410 Grognard I was a single seat low-level ground attack experimental monoplane prototype,powered by two Hispano-Suiza (built under license RR) Nene 101 turbojet engines
SE-2411 Grognard was a developed version from SE-2410,powered by Rolls Royce Nene 102 turbojet engines,need
confirm
SE-2412 Grognard maybe a misprint
SE-2415 Grognard II was a two-seat as a development version,that included a stretched fuselage incorporating a
raised cockpit with a bubble canopy and reduced 32˚ wing sweep back,powered by the same engines
SE-2416 Grognard was a single seat strike aircraft Project version,with four HS 603 30mm machine guns,also
the same engines
SE-2417 Grognard was a SE-2415,re-engine with Tay or Verdon turbojets,and fitted with eight 20mm guns,Project
SE-2418 Grognard was a single seat version,this design mated a highly swept wing SE-2410 and SE-2415 fuselage,
with two 30mm guns,and the same engines,Project
SE-2418/I Grognard was a version,powered by two Snecma ATAR 101F turbojet engine,mounted side-by-side,
and two 30mm guns,Project
SE-2419 Grognard was a direct adaption of SE-2418 with two Rolls Royce Nene turbojets,and two 30mm guns,
Project
SE-2420 Grognard III was based on third prototype (SE-2415) with thin wings,with two Tay turbojets,never
completed
SE-2421 Grognard was a two-seat long-range all-weather fighter Project,based on SE-2420 and same engines
SE-2422 Grognard was a single seat strike aircraft Project,with thin wings and featured a revised air-intakes
(lesser bulky but wider),maybe with RR Nene engines
SE-2422R Grognard was a single seat recce version of SE-2422,with cameras in place of gun bay
SE-2423 Grognard was a design version,mated the fuselage of SE-2418 with the wings of SE-2415,Project
SE-2424 Grognard was anther version of SE-2418,but with Snecma Vulcain P-150 engines with post combustion
SE-2450 Grognard was a simplified SE-2400/I,side-by-side two-seat with bubble canopy and pursuit radar,and
powered by two Hispano-Suiza Nene turbojets,mounted beside the fuselage with wing roots,Project
SE-2500 was a designation mentioned as similar to the X-201.02.01,jet airliner Project
SE-2600 was missile Project
SE-2700,SE-2800 & SE-2900 were unknown designs,maybe not used
SE-3000 was a heavy two rotor transport helicopter project (also allocated to former Focke-Achgelis Fa 223)
SE-3001 was a flying model of the SE-3100
SE-3010 was unknown Project,need confirm
SE-3100 was a twin-engine single-rotor large helicopter Project,with unusual twin, angled tail rotors
SE-3101 was an experimental sub-scale prototype version of SE 3100, first French helicopter
SE-3110 was a two-seat experimental light helicopter,powered by one 200 hp Salmson 9 Nh engine,with unusual twin, angled tail rotors
SE-3111 was a variant Project fitted with rotors larger diameter tail (2.80 m instead 2.40 m),based on SE-3110
SE-3120 Alouette was a single seat crew and two seat utility helicopter,powered by one 200 hp Salmson 9 Nh engine
SE-3130 Alouette II was enlarge version of SE-3120,with one crew and four seat,utility and multi-role helicopter,
powered by one 530 hp Turbomeca Artouste IIC6 turboshaft engine
SE-3131 Gouverneur was a version of Alouette
SE-3140 was Alouette II modified with shorter main rotor blades anf 400 hp Turbomeca Turmo turboshaft
engine
SE-3150 Lama was Allouette II,fitted with larger main rotor,3-blade tail rotor and powered by one 500 hp Turbomeca
Artouste III turboshaft engine
SE-3160 Allouette III was a redesigned Allouette II with all-metal monocoque fuselage,and a fully enclosed seven-seat cabin and fixed tricycle undercarriage,powered by 870 hp Turbomeca Artouste IIIB turboshaft engine
SE-3164 was Allouette II with stepped windshield and nose-mounted 20mm gun,prototype
SE-3170 was unknown Project
SE-3180 Allouette was Allouette II fitted with 450 hp Turbomeca Artouste II turbine for high altitude operation,
prototype
SE-3190 was SE-3160 fitted with 600 hp Turbomeca Astazou XIV turboshaft engine,prototype
SE-3200 Frelon was a heavy transport helicopter with single four-blade main rotor,powered by three 750 hp
Turbomeca Turmo IIIB turboshaft engines,positioned in housing on top of fuselage
SA-3210 Super Frelon was developed from SE-3200,with boat hull and outrigger floats,rear loading doors,boom tail,
six-blade main rotor driven three 1320 hp Turbomeca Turmo IIIC turboshaft engines
SA-3220 Super Frelon was enlarge version of total mass 10 ton,with single five-blade main rotor,the waterproof
hull was extended at the front by a bow and bent tail (foldable) used to raise the anti-torque rotor,powered by
three 1250 hp Turbomeca Turmo IIIC turboshaft engines,Project
SA-3230 Super Frelon was a Project version of SE-3220,its empty mass was 4,800 kg and its total takeoff weight was only 9 ton,and powered by only two 1320 hp Turbomeca Turmo IIIC turboshaft engines
SA-330 Puma was a medium-lift 20 troop military helicopter with retractable tricycle undercarriage and single
four-blade main rotor ,powered by two 1320 hp Turbomeca Turmo IIIC4 turboshaft engines
SA-340 Gazelle was a light five-seat multi-role helicopter,with streamlined fuselage,tail rotor,three-blade main
rotor,powered by one Turbomeca Astazou IIN2 turboshaft engine
SE-4000 was a high-wing amphibian flying boat light transport Project,powered by one 450 hp Mathis 16G
pusher engine,mounted above the wing
SE-4010 & SE-4020 maybe unknown Project versions of SE-4000
SE-4030 was a high-wing amphibian flying boat light transport Project,enlarge version of SE-4000,powered by two Armstrong Siddeley Cheetah or P&W engines,in tractor position
SE-4100 was a first French rocket, Project only
SE-4101,SE-4102,SE-4103,SE-4104,SE-4110,SE-4111,SE-4112,SE-4113,SE-4114,SE-4115,SE-4116,SE-4117,SE-4118 &
SE-4119 were a variants of SE-4100
SE-4120 & SE-4130 were unknown
SE-4140 was a variant of SE-4100
SE-4200 was a first operational ramjet-powered ground-to-ground missile
SE-4201 was a variant of SE-4200
SE-4202 was a variant of SE-4200
SE-4204 was a variant of SE-4200
SE-4205 was a variant of SE-4200
SE-4207 was a variant of SE-4200
SE-4208 was a variant of SE-4200
SE-4209 was a variant of SE-4200
SE-4210 was a variant of SE-4200
SE-4211 was a variant of SE-4200
SE-4212 was a variant of SE-4200
SE-4220 was a variant of SE-4200
SE-4230 was a variant of SE-4200
SE-4263 was a variant of SE-4200
SE-4280 was a variant of SE-4200
SE-4299 was a target,need Info
SE-4300 was a variant of SE-4100 with French radar
SE-4400 was a ramjet-powered ground-to-air missile with same radar as above
SE-4402 was a record-breaking variant of above
SE-4500 was a enlarged ramjet-powered version of the SE-4200 intended to carry a 700-kg bomb at a distance of
130 kms
SE-4600.SE-4700,SE-4800 & SE-4900 probably not used
SE-5000 Baroudeur was a single seat high-wing lightweight strike fighter monoplane,powered by one Snecma
ATAR 101D turbojet engine
SE-5000-01 Baroudeur was a first prototype built,powered by one Snecma ATAR 101C turbojet engine
SE-5000-02 Baroudeur was a second prototype built,with some modifications
SE-5001 Baroudeur maybe it was a version with two addition Rolls Royce Soar booster engines
SE-5002 Baroudeur A was a smaller version,powered by one Bristol Siddeley Orpheus II turbojet engine
SE-5003 Baroudeur was a pre-series version,that incorporated test for many engines,ATAR E3,E4 & D3
SE-5004 Baroudeur was a version,powered by one Snecma ATAR E4 engine
SE-5005 Baroudeur maybe a misprint in L+K magazine,as a version with additions two rocket powered engines
SE-5008 Baroudeur was a proposed series version with Snecam ATAR 8 engine
SE-5008 VS Baroudeur was anther Project with blown wing,powered by one Snecma ATAR 8 engine
SE-5010 Baroudeur L was a light tactical support variant
SE-5012 Baroudeur was a proposed series version with one Bristol Siddeley Orpheus engine
SE-5013 Baroudeur was based on Baroudeur A,with Bristol Siddeley Orpheus engine,and a blown wing,Project
SE-5020 Baroudeur S was a lightened airframe Project with Snecma ATAR 101E engine
SE-5030 Baroudeur R was a Project version,powered y one Snecma M17 engine
SE-5040 Baroudeur O was a Project of lightweight version,powered by one Bristol Siddeley Orpheus
SE-5050 Baroudeur was developed from SE 5091,with blown wing and Snecma ATAR engine,Project
SE-5060 Baroudeur A/II maybe was a lighter version with thin wing,also fitted with two addition Rolls Royce Soar booster engines
SE-5070 Baroudeur M maybe was a naval version to use from aircraft carrier,project,need confirm
SE-5091 Baroudeur was a Project in collaboration with Fiat
- ANY ADDITIONS OR CORRECTIONS ARE WELCOME