Nord Aviation and SNCAN designations
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- Joined
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- Messages
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- Reaction score
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The SNCAN or Nord first series;
Nord (SNCAC) NC-700 Martinet
Nord (NC-)854 (numbering taken over from SNCAC's NC- list)
Nord (NC-)855 variant with Praga-D engine
Nord (NC-)856 variant with Walter Minor 4.11W engine
Nord (NC-)856A Norvigie
Nord (NC-)856H variant with Régnier engine; belonged to Prince Rainier of Monaco (1 built)
Nord (NC-)856N Norclub twin-fin commercial variant
Nord (NC-)858 variant with Continental C90-12F engine
Nord (NC-)858.S conversion of NC 853 with Continental C-90 engine
N.1000 was a French-built Me.108b four-seat low-wing cabin monoplane with retractable tailwheel u/c and Argus AS.10B engine
N.1001 Pingouin I was N.1000 with 220 h.p. Renault 6Q.11 engine
N.1002 Pingouin II was N.1001 with Renault 6Q.10 engine
N.1003 & N.1004 Pingouin was a version Projects,need confirm
N.1100 Noralpha was N.1000 with larger fuselage, retractable tricycle u/c and 240 hp Argus As.10C engine
N.1101 Ramier I was N.1100 with right-hand turning Renault 6Q.10 engine
N.1102 Ramier II was N.1100 with left-hand turning Renault 6Q.11 engine
N.1103 Ramier ? was unknown version,need Info
N.1104 Noralpha was experimental N.1101 (c/n 61) with 240 hp Potez 6DO engine
N.1110 was a two experimental N.1101s fitted with Turbomeca Astazou turboprop engine,1959
N.1150 was an executive jet Project,formerly SNCAC NC.1150
N.1200 Norecrin was all-metal 2/3 seat tourer based on N. 1000 with retractable tricycle u/c and 100 h.p Mathis G4R engine
N.1201 Norecrin I was production three-seat Norecrin with large rear window and 140 hp Renault 4PO1 engine
N.1202 Norecrin was N.1201 F-BBKA (c/n 02) fitted with 160 h.p. Potez 4DO1 engine
N.1203 Norecrin II was a Four-seat Norecrin with 135 h.p. Regnier 4L00 engine.
N.1203 Norecrin III was Norecrin II with modified undercarriage
N.1203 Norecrin IV was Norecrin II with 170 h.p. Regnier 4L02 engine and constant speed propeller
N.1203 Norecrin V was a military two-seat Norecrin with 170 hp Regnier 4L02 engine and machine guns and rockets
N.1203 Norecrin VI was Norecrin III with 145 hp Regnier 4L14 engine
N.1204 Norecrin was N.1203 with 125 Continental engine
N.1220 was a 2/3 three trainer low-wing monoplane,powered by one 140 hp Renault 4Pei engine
N.1221 Norélan was a prototype with 180 hp Mathis 8G20 inverted Vee engine,later converted to N.1222.
N.1222 Norélan was a prototype re-engined with a 180hp Regnier 4L02 inline engine
N.1223 Norélan was a version,powered by a 240hp Argus As 10C inverted Vee engine
N.1224 & N.1225 Norélan were unknown Projects
N.1226 Norélan was an engine-testbed for the 240hp Potez 6D-0 inline engine
N.1300 Norbaby was a single seat high-wing training glider monoplane,a licence built Schneider Grunau Baby
N.1400 Noroît was a cantilever gull-wing recce and sea rescue flying boat monoplane,powered by two 1600 hp Gnome-Rhône 14R radial engines
N.1401 Noroît was a variant with Snecma Jumo engines
N.1402 Noroît was a variant with Arsenal engines
N.1402 (Arsenal) Gerfaut A was a single seat delta-wing research aircraft,powered by a ramjet with auxiliaryTurboméca turbojet, and middle-set wings
N.1402 (Arsenal) Gerfaut B was a version,powered by ATAR 101C turbojet engine
N.1403 (Arsenal) Gerfaut was a version,powered by a combined ramjet / turbojet powerplant and middle-set wings
N.1404 (Arsenal) Gerfaut was a Project version,powered by a combined ramjet / turbojet powerplant and low-set wings
N.1405 (Arsenal) Gerfaut II was a version,powered by an ATAR 101 turbojet powerplant and low-set wings
N.1480 was a shoulder wing twin-boom heavy transport and cargo monoplane Project,powered by two engines
N.1500 Noréclair was a mid-wing twin-engined dive bomber and anti-submarine warfare aircraft,powered by two 1600 hp Gnome-Rhône 14R-25 engines
N.1501 Noréclair was a version,powered by Bristol Hercules engines,
N.1510 Noréclair was a version,but powered by RR Nene turbojet engines,never completed
N.1500 (Arsenal) Griffon I was a single seat delta-wing canard ramjet powered research or fighter aircraft,powered by Nord Stato-Réacteur Ramjet engine
N.1500 (Arsenal) Griffon II was a second aircraft fitted with the definitive turbo-ramjet powerplant
N.1501 (Arsenal) was a Project developed from Arsenal 1402A Gerfaut
N.1502 (Arsenal) Guepard was an experimental fighter Project,developed from Griffon,powered by ATAR 101F engine
N.1520 Griffon III/1 was a developed Project version,with new shape and 3 Mach capacity,powered by one Super ATAR 20 ramjet engine
N.1520 Griffon III/2 was a developed Project version of Griffon III/1,but powered by two Super ATAR 90 ramjet engines
N.1540 was a single seat low-wing jet interceptor Project for 1953 contest,powered by one HS Nene engine or ATAR 101 E2 engine
N.1541 was a Project version,powered by one ATAR 101 M13 turbojet engine
N.1600 was a single seat experimental fighter and research mid-swept-wing Project,with T-tail,powered by two Reteau B-120 SRA 1 turbojet engines
N.1601 was developed version with normal rear wing,powered by two Rolls Royce Derwent V turbojet engines
N.1602 & N.1610 maybe a developed Project versions,need confirm
N.1620 was a two-seat straight wing fighter/bomber Project,based on N.1601,also powered by two turbojets
N.1700 Norélic was a two-seat research helicopter,powered by one 160 Mathis GR7 radial engine
N.1710 was a single seat helicopter,a refined version of N.1700,which shared a similar control system,though horizontal surfaces were added within the shroud for pitch control,powered by one 75 hp Nathis 4C20 engine
N.1720,N.1730 & N.1740 maybe not used
N.1750 Norelfe was a three-seat helicopter,based on N.1700,had a single main rotor, with torque control through a movable duct at the end of the tailboom,powered by one Turbomeca Artouste turboshaft engines
N.1800A was a six-seat heavy bomber Project,looks like Boeing B-29,had a high-wing shape and powered by maybe four piston engines
N.1800B was a Project developed from N.1800A,but a larger aircraft,and powered by turboprop engines
N.1800C was a Project version of N.1800A,but powered a turbojet engines
N.1910 (Arsenal) was a single seat delta wing interceptor Project,powered by one Turbomeca Marbore II turbojet engine.
N.2000 was a single seat high-wing glider,a licence built DFS Olympia Meise
N.2100 Norazur was a high-wing civil transport cantilever monoplane with a retractable tricycle landing gear,powered by two 420 hp Potez 8D-03 inverted, air-cooled V-8 piston engines in pusher configuration
N.2101 Norazur was a prototype with alternate 390 hp Bearn 6D-07 inverted, air-cooled V-6 piston engines in pusher configuration
N.2102 Norazur was a Project version with two Snecma 12S engines in tractor configuration
N.2200 was a single seat low-wing naval fighter monoplane,powered by one HS Nene 102 turbojet engine
N.2301 (Arsenal) was a single seat swept-wing jet fighter Project,formerly SFECMAS 2301
N.2302 (Arsenal) was a Project developed from ARS/Nord 2301,no details.
N.2400 maybe a twin jet research bomber Project,need confirm
N.2500 Noratlas was a twin-boom military medium transport monoplane,powered by two 1600 hp Gnome-Rhône 14R engines
N.2501 Noratlas was a production version for the French Air Force, powered by Snecma-manufactured Hercules 739 radial piston engines
N.2502 Noratlas was a civil transport version for Union Aéromaritime de Transport, powered by two Turbomeca Marboré II auxiliary turbojets and two 1650-hp Bristol Hercules 758/759 radial engines
N.2503 Noratlas was a re-engined version with two 1864-kW (2,500-hp) Pratt & Whitney R-2800-CB17 radial
piston engines
N.2504 Noratlas was a modification of the Nord 2502 intended for antisubmarine warfare training role with the French Navy
N.2505 Noratlas was a modified Nord 2502 intended for antisubmarine warfare,cancelled not built
N.2506 Noratlas was a special modification of Nord 2502 to improve STOL performance and performance under heavy load for use as an assault transport
N.2507 Noratlas was a modified Nord 2502 intended for search and rescue role, with 12-hour endurance or greater, never passed the planning stage
N.2508 Noratlas was a modified Nord 2503, powered by two 1864-kW (2,500-hp) Pratt & Whitney R-2800-CB17 radial piston engines and two Turbomeca Marboré IIE auxiliary turbojets added; highly capable
N.2509 Noratlas was a anti-submarine aircraft Project
N.2510 Noratlas was a unbuilt anti-submarine warfare version
N.2520 Noratlas was an enlarged Nord 2502 with better cargo capacity
N.2540 was a single seat jet interceptor Project,intended for 1953 Contest,powered by one Bristol Siddeley Orpheus turbojet engine
N.2600 was high-wing medium airliner Project,powered by two Rolls Royce Dart turboprop engines
N.2700 was a mid-wing high seas monoplane Project,powered by four turboprop engines
N.2800 was a three-seat low-wing basic trainer monoplane,powered by one 240 hp Salmson Argus As-10C engine
N.2900 was a high-wing attack recce monoplane Project,powered b two ATAR turbojet engines
N.3000A was a jet airliner Project to compete SNCASE Caravelle,powered by three ATAR or RR Avon turbojet engines,had a low arrow wing
N.3000B was a jet airliner Project to compete SNCASE Caravelle,but had arrowless wing shape,and powered by four turbojet engines
N.3100 was a developed from N.2501,but completely different,had a low-wing,simple tail unit,the fuselage at the rear does not end with the cone classic and crew of five,longer 32.20m and span 36.10m,powered by two Bristol
Proteus (750) 4150 hp turboprop engines + two Marbore turbojet engines,Project
N.3200 was a two-seat low-wing primary trainer monoplane,powered by one 240 hp Salmson 8AS-04 engine
N.3201 was a version,powered by one 170 hp Regnier 4L-22 engine
N.3202 was a production variant,powered by one 240 hp Potez 4D-32 engine
N.3210 & N.3211 maybe unknown variants or not built
N.3212 was a redesignation for 3202s fitted with radio compass and equipped for instrument flight training
N.3300 was a COIN aircraft Project,was submitted to 1956 competition
N.3400 Norbarbe was a two-seat observation and casualty-evacuatio high-wing monoplane,powered by one 240 hp Potez 4D-30 engine
N.3500 was a civil/military co-operation medium transport aircraft Project,in class of Hurel-Dubois HD.150 and SIPA S.271
N.3540 was a single seat jet interceptor Project for 1953 contest,powered by one ATAR engine
N.3541 was a single seat jet interceptor Project for 1953 contest,powered by two RR Orpheus engines
N.3600 Harpoon was a tandem two-seat low-wing strike,ground attack and trainer aircraft Project,intended for ECAT program,powered by two Rolls Royce RB.172-49R or Snecma M45B turbojet engines
N.3700,N.3800,N.3900,N.4000 & N.4100 were unknown designs
N.4200 was a single seat high delta wing supersonic ground attack VTOL aircraft Project,powered by one Bristol BE.53/11 turbojet engine
N.4210 was a single seat high delta wing supersonic ground attack VTOL aircraft Project,powered by one Bristol BE.53/5 or BE.53/6 Turbojet engine
N.4300 was a single seat high delta wing supersonic ground attack VTOL aircraft Project,powered by one Bristol BE.53/5HR + one Bristol BE.59/7 lift fan turbojet engines
N.4400 was a single seat supersonic ground attack VTOL aircraft Project,developed from N.4210,with new shape,looks like Hawker P.1127,powered by one Bristol BE.53/16 turbojet engine
N.4500 to N.4900 were unknown designs
N.5000 Harpoon was a single seat delta wing canard supersonic interceptor Project,powered by one Nene turbojet engine
N.5010 Harpoon was single seat delat wing canard light strike and ground attack Project.a scale down configuration of N.5000,powered by two Gabizo turbojet engines
N.5101 (Arsenal) was air-to-air missile = AA-10
N.5102 (Arsenal) was air-to-air missile = AA-10
N.5103 (Arsenal) was air-to-air missile = AA-20
N.5104 (Arsenal) was air-to-air missile = AA-25
N.5110 (Arsenal) was air-to-air missile = AS-20
N.5201 (Arsenal) was air-to-air missile = SS-10
N.5202 (Arsenal) was air-to-air missile = SS-10
N.5203 (Arsenal) was air-to-air missile = SS-10
N.5210 (Arsenal) was air-to-air missile = SS-11
N.5301 (Arsenal) was air-to-air missile = ACAM
N.5401 (Arsenal) was unknown design
N.5501 (Arsenal) was air-to-air missile = CT-10
N.5510 (Arsenal) was air-to-air missile = CT-20
N.6000 was a high-wing very heavy transport monoplane Project (looks like Lockheed C-5 Galaxy),powered
by four turbojet engines
Any additions or corrections are welcome
Nord (SNCAC) NC-700 Martinet
Nord (NC-)854 (numbering taken over from SNCAC's NC- list)
Nord (NC-)855 variant with Praga-D engine
Nord (NC-)856 variant with Walter Minor 4.11W engine
Nord (NC-)856A Norvigie
Nord (NC-)856H variant with Régnier engine; belonged to Prince Rainier of Monaco (1 built)
Nord (NC-)856N Norclub twin-fin commercial variant
Nord (NC-)858 variant with Continental C90-12F engine
Nord (NC-)858.S conversion of NC 853 with Continental C-90 engine
N.1000 was a French-built Me.108b four-seat low-wing cabin monoplane with retractable tailwheel u/c and Argus AS.10B engine
N.1001 Pingouin I was N.1000 with 220 h.p. Renault 6Q.11 engine
N.1002 Pingouin II was N.1001 with Renault 6Q.10 engine
N.1003 & N.1004 Pingouin was a version Projects,need confirm
N.1100 Noralpha was N.1000 with larger fuselage, retractable tricycle u/c and 240 hp Argus As.10C engine
N.1101 Ramier I was N.1100 with right-hand turning Renault 6Q.10 engine
N.1102 Ramier II was N.1100 with left-hand turning Renault 6Q.11 engine
N.1103 Ramier ? was unknown version,need Info
N.1104 Noralpha was experimental N.1101 (c/n 61) with 240 hp Potez 6DO engine
N.1110 was a two experimental N.1101s fitted with Turbomeca Astazou turboprop engine,1959
N.1150 was an executive jet Project,formerly SNCAC NC.1150
N.1200 Norecrin was all-metal 2/3 seat tourer based on N. 1000 with retractable tricycle u/c and 100 h.p Mathis G4R engine
N.1201 Norecrin I was production three-seat Norecrin with large rear window and 140 hp Renault 4PO1 engine
N.1202 Norecrin was N.1201 F-BBKA (c/n 02) fitted with 160 h.p. Potez 4DO1 engine
N.1203 Norecrin II was a Four-seat Norecrin with 135 h.p. Regnier 4L00 engine.
N.1203 Norecrin III was Norecrin II with modified undercarriage
N.1203 Norecrin IV was Norecrin II with 170 h.p. Regnier 4L02 engine and constant speed propeller
N.1203 Norecrin V was a military two-seat Norecrin with 170 hp Regnier 4L02 engine and machine guns and rockets
N.1203 Norecrin VI was Norecrin III with 145 hp Regnier 4L14 engine
N.1204 Norecrin was N.1203 with 125 Continental engine
N.1220 was a 2/3 three trainer low-wing monoplane,powered by one 140 hp Renault 4Pei engine
N.1221 Norélan was a prototype with 180 hp Mathis 8G20 inverted Vee engine,later converted to N.1222.
N.1222 Norélan was a prototype re-engined with a 180hp Regnier 4L02 inline engine
N.1223 Norélan was a version,powered by a 240hp Argus As 10C inverted Vee engine
N.1224 & N.1225 Norélan were unknown Projects
N.1226 Norélan was an engine-testbed for the 240hp Potez 6D-0 inline engine
N.1300 Norbaby was a single seat high-wing training glider monoplane,a licence built Schneider Grunau Baby
N.1400 Noroît was a cantilever gull-wing recce and sea rescue flying boat monoplane,powered by two 1600 hp Gnome-Rhône 14R radial engines
N.1401 Noroît was a variant with Snecma Jumo engines
N.1402 Noroît was a variant with Arsenal engines
N.1402 (Arsenal) Gerfaut A was a single seat delta-wing research aircraft,powered by a ramjet with auxiliaryTurboméca turbojet, and middle-set wings
N.1402 (Arsenal) Gerfaut B was a version,powered by ATAR 101C turbojet engine
N.1403 (Arsenal) Gerfaut was a version,powered by a combined ramjet / turbojet powerplant and middle-set wings
N.1404 (Arsenal) Gerfaut was a Project version,powered by a combined ramjet / turbojet powerplant and low-set wings
N.1405 (Arsenal) Gerfaut II was a version,powered by an ATAR 101 turbojet powerplant and low-set wings
N.1480 was a shoulder wing twin-boom heavy transport and cargo monoplane Project,powered by two engines
N.1500 Noréclair was a mid-wing twin-engined dive bomber and anti-submarine warfare aircraft,powered by two 1600 hp Gnome-Rhône 14R-25 engines
N.1501 Noréclair was a version,powered by Bristol Hercules engines,
N.1510 Noréclair was a version,but powered by RR Nene turbojet engines,never completed
N.1500 (Arsenal) Griffon I was a single seat delta-wing canard ramjet powered research or fighter aircraft,powered by Nord Stato-Réacteur Ramjet engine
N.1500 (Arsenal) Griffon II was a second aircraft fitted with the definitive turbo-ramjet powerplant
N.1501 (Arsenal) was a Project developed from Arsenal 1402A Gerfaut
N.1502 (Arsenal) Guepard was an experimental fighter Project,developed from Griffon,powered by ATAR 101F engine
N.1520 Griffon III/1 was a developed Project version,with new shape and 3 Mach capacity,powered by one Super ATAR 20 ramjet engine
N.1520 Griffon III/2 was a developed Project version of Griffon III/1,but powered by two Super ATAR 90 ramjet engines
N.1540 was a single seat low-wing jet interceptor Project for 1953 contest,powered by one HS Nene engine or ATAR 101 E2 engine
N.1541 was a Project version,powered by one ATAR 101 M13 turbojet engine
N.1600 was a single seat experimental fighter and research mid-swept-wing Project,with T-tail,powered by two Reteau B-120 SRA 1 turbojet engines
N.1601 was developed version with normal rear wing,powered by two Rolls Royce Derwent V turbojet engines
N.1602 & N.1610 maybe a developed Project versions,need confirm
N.1620 was a two-seat straight wing fighter/bomber Project,based on N.1601,also powered by two turbojets
N.1700 Norélic was a two-seat research helicopter,powered by one 160 Mathis GR7 radial engine
N.1710 was a single seat helicopter,a refined version of N.1700,which shared a similar control system,though horizontal surfaces were added within the shroud for pitch control,powered by one 75 hp Nathis 4C20 engine
N.1720,N.1730 & N.1740 maybe not used
N.1750 Norelfe was a three-seat helicopter,based on N.1700,had a single main rotor, with torque control through a movable duct at the end of the tailboom,powered by one Turbomeca Artouste turboshaft engines
N.1800A was a six-seat heavy bomber Project,looks like Boeing B-29,had a high-wing shape and powered by maybe four piston engines
N.1800B was a Project developed from N.1800A,but a larger aircraft,and powered by turboprop engines
N.1800C was a Project version of N.1800A,but powered a turbojet engines
N.1910 (Arsenal) was a single seat delta wing interceptor Project,powered by one Turbomeca Marbore II turbojet engine.
N.2000 was a single seat high-wing glider,a licence built DFS Olympia Meise
N.2100 Norazur was a high-wing civil transport cantilever monoplane with a retractable tricycle landing gear,powered by two 420 hp Potez 8D-03 inverted, air-cooled V-8 piston engines in pusher configuration
N.2101 Norazur was a prototype with alternate 390 hp Bearn 6D-07 inverted, air-cooled V-6 piston engines in pusher configuration
N.2102 Norazur was a Project version with two Snecma 12S engines in tractor configuration
N.2200 was a single seat low-wing naval fighter monoplane,powered by one HS Nene 102 turbojet engine
N.2301 (Arsenal) was a single seat swept-wing jet fighter Project,formerly SFECMAS 2301
N.2302 (Arsenal) was a Project developed from ARS/Nord 2301,no details.
N.2400 maybe a twin jet research bomber Project,need confirm
N.2500 Noratlas was a twin-boom military medium transport monoplane,powered by two 1600 hp Gnome-Rhône 14R engines
N.2501 Noratlas was a production version for the French Air Force, powered by Snecma-manufactured Hercules 739 radial piston engines
N.2502 Noratlas was a civil transport version for Union Aéromaritime de Transport, powered by two Turbomeca Marboré II auxiliary turbojets and two 1650-hp Bristol Hercules 758/759 radial engines
N.2503 Noratlas was a re-engined version with two 1864-kW (2,500-hp) Pratt & Whitney R-2800-CB17 radial
piston engines
N.2504 Noratlas was a modification of the Nord 2502 intended for antisubmarine warfare training role with the French Navy
N.2505 Noratlas was a modified Nord 2502 intended for antisubmarine warfare,cancelled not built
N.2506 Noratlas was a special modification of Nord 2502 to improve STOL performance and performance under heavy load for use as an assault transport
N.2507 Noratlas was a modified Nord 2502 intended for search and rescue role, with 12-hour endurance or greater, never passed the planning stage
N.2508 Noratlas was a modified Nord 2503, powered by two 1864-kW (2,500-hp) Pratt & Whitney R-2800-CB17 radial piston engines and two Turbomeca Marboré IIE auxiliary turbojets added; highly capable
N.2509 Noratlas was a anti-submarine aircraft Project
N.2510 Noratlas was a unbuilt anti-submarine warfare version
N.2520 Noratlas was an enlarged Nord 2502 with better cargo capacity
N.2540 was a single seat jet interceptor Project,intended for 1953 Contest,powered by one Bristol Siddeley Orpheus turbojet engine
N.2600 was high-wing medium airliner Project,powered by two Rolls Royce Dart turboprop engines
N.2700 was a mid-wing high seas monoplane Project,powered by four turboprop engines
N.2800 was a three-seat low-wing basic trainer monoplane,powered by one 240 hp Salmson Argus As-10C engine
N.2900 was a high-wing attack recce monoplane Project,powered b two ATAR turbojet engines
N.3000A was a jet airliner Project to compete SNCASE Caravelle,powered by three ATAR or RR Avon turbojet engines,had a low arrow wing
N.3000B was a jet airliner Project to compete SNCASE Caravelle,but had arrowless wing shape,and powered by four turbojet engines
N.3100 was a developed from N.2501,but completely different,had a low-wing,simple tail unit,the fuselage at the rear does not end with the cone classic and crew of five,longer 32.20m and span 36.10m,powered by two Bristol
Proteus (750) 4150 hp turboprop engines + two Marbore turbojet engines,Project
N.3200 was a two-seat low-wing primary trainer monoplane,powered by one 240 hp Salmson 8AS-04 engine
N.3201 was a version,powered by one 170 hp Regnier 4L-22 engine
N.3202 was a production variant,powered by one 240 hp Potez 4D-32 engine
N.3210 & N.3211 maybe unknown variants or not built
N.3212 was a redesignation for 3202s fitted with radio compass and equipped for instrument flight training
N.3300 was a COIN aircraft Project,was submitted to 1956 competition
N.3400 Norbarbe was a two-seat observation and casualty-evacuatio high-wing monoplane,powered by one 240 hp Potez 4D-30 engine
N.3500 was a civil/military co-operation medium transport aircraft Project,in class of Hurel-Dubois HD.150 and SIPA S.271
N.3540 was a single seat jet interceptor Project for 1953 contest,powered by one ATAR engine
N.3541 was a single seat jet interceptor Project for 1953 contest,powered by two RR Orpheus engines
N.3600 Harpoon was a tandem two-seat low-wing strike,ground attack and trainer aircraft Project,intended for ECAT program,powered by two Rolls Royce RB.172-49R or Snecma M45B turbojet engines
N.3700,N.3800,N.3900,N.4000 & N.4100 were unknown designs
N.4200 was a single seat high delta wing supersonic ground attack VTOL aircraft Project,powered by one Bristol BE.53/11 turbojet engine
N.4210 was a single seat high delta wing supersonic ground attack VTOL aircraft Project,powered by one Bristol BE.53/5 or BE.53/6 Turbojet engine
N.4300 was a single seat high delta wing supersonic ground attack VTOL aircraft Project,powered by one Bristol BE.53/5HR + one Bristol BE.59/7 lift fan turbojet engines
N.4400 was a single seat supersonic ground attack VTOL aircraft Project,developed from N.4210,with new shape,looks like Hawker P.1127,powered by one Bristol BE.53/16 turbojet engine
N.4500 to N.4900 were unknown designs
N.5000 Harpoon was a single seat delta wing canard supersonic interceptor Project,powered by one Nene turbojet engine
N.5010 Harpoon was single seat delat wing canard light strike and ground attack Project.a scale down configuration of N.5000,powered by two Gabizo turbojet engines
N.5101 (Arsenal) was air-to-air missile = AA-10
N.5102 (Arsenal) was air-to-air missile = AA-10
N.5103 (Arsenal) was air-to-air missile = AA-20
N.5104 (Arsenal) was air-to-air missile = AA-25
N.5110 (Arsenal) was air-to-air missile = AS-20
N.5201 (Arsenal) was air-to-air missile = SS-10
N.5202 (Arsenal) was air-to-air missile = SS-10
N.5203 (Arsenal) was air-to-air missile = SS-10
N.5210 (Arsenal) was air-to-air missile = SS-11
N.5301 (Arsenal) was air-to-air missile = ACAM
N.5401 (Arsenal) was unknown design
N.5501 (Arsenal) was air-to-air missile = CT-10
N.5510 (Arsenal) was air-to-air missile = CT-20
N.6000 was a high-wing very heavy transport monoplane Project (looks like Lockheed C-5 Galaxy),powered
by four turbojet engines
Any additions or corrections are welcome
Last edited:
- Joined
- 26 May 2006
- Messages
- 33,589
- Reaction score
- 13,722
Hi,
here is a clue for Nord N.1003;
commons.wikimedia.org
here is a clue for Nord N.1003;
File:Nord N.1003 (Messerschmitt Bf108 Taifun) (5381504337).jpg - Wikimedia Commons
- Joined
- 26 May 2006
- Messages
- 33,589
- Reaction score
- 13,722
Here is the second series;
N.100,N.101 & N.102 were a hovercraft
N.200 was unknown design
N.300 was a hovercraft
N.400A was a low-wing business jet executive monoplane Project,powered by two turbojets,mounted at
the rear side of the fuselage,almost from middle
N.400B was a low-wing business jet executive monoplane Project,powered by two turbojets,mounted
immediately under the wings
N.500 Early was a tandem two-seat parasol wing tilt ducted fan VTOL research monoplane Project
N.500 Cadet was a two seat at tilt ducted fan VTOL research high-wing monoplane prototype,powered
two 316 hp Allison T63 turboshaft engines
N.500/II Cadet was a four-seat version of N.500,but powered by two 350 hp Oredon 111 engines
N.500B Helcade was a single seat version of N.500,also experimental aircraft,Project
N.500 Militaire was military version Project,intended for Navy,had a completed new tail unit
N.500 Estocade was a single seat ground attack version,with modern new configuration,Project
N.500 Rocade was a 40 passenger large version of N.500,had a V-tail,powered by four 1100 hp
Turboméca Turmo-IIIC engines
N.501 Helcade was a tandem two-seat attack and ASW Project,had a new shape for ducted fan and
drawn fuselage,powered by two 2100 hp Lycoming T55 engines
N.501 was a 8 passenger large version of N.500,powered by two 2650 hp Lycoming T55 turboshaft engines
N.510 was a tethered platform for use in battlefield observation,could be raise to 300m
N.511 was a version of N.510,could be raise to 1000m
N.520 was a heavy hovercraft
N.600/I was a very large transport high-wing monoplane,powered by eight turbojet engines,mounted
each four in one pod under each wing
N.600/II was a low-wing jet airliner Project,powered by four turbojet engines,mounted at the side
of the rear fuselage,one above one in each way
SN.600 Diplomate was a low-wing business jet monoplane aircraft,powered by two Pratt & Whitney Canada
JT15D-1 turbofan engines,each one mounted at the side of the rear fuselage part,developed with Sud-Aviation
SN.601 Corvette was a production version with longer fuselage than SN.600,powered by two JT15D-4 turbofan
engines,also with Sud-Aviation
SN.602 Corvette was a developed version by Aerospatiale,but powered by two Snecma Turbomeca Larzac 03 turbofan engines
N.100,N.101 & N.102 were a hovercraft
N.200 was unknown design
N.300 was a hovercraft
N.400A was a low-wing business jet executive monoplane Project,powered by two turbojets,mounted at
the rear side of the fuselage,almost from middle
N.400B was a low-wing business jet executive monoplane Project,powered by two turbojets,mounted
immediately under the wings
N.500 Early was a tandem two-seat parasol wing tilt ducted fan VTOL research monoplane Project
N.500 Cadet was a two seat at tilt ducted fan VTOL research high-wing monoplane prototype,powered
two 316 hp Allison T63 turboshaft engines
N.500/II Cadet was a four-seat version of N.500,but powered by two 350 hp Oredon 111 engines
N.500B Helcade was a single seat version of N.500,also experimental aircraft,Project
N.500 Militaire was military version Project,intended for Navy,had a completed new tail unit
N.500 Estocade was a single seat ground attack version,with modern new configuration,Project
N.500 Rocade was a 40 passenger large version of N.500,had a V-tail,powered by four 1100 hp
Turboméca Turmo-IIIC engines
N.501 Helcade was a tandem two-seat attack and ASW Project,had a new shape for ducted fan and
drawn fuselage,powered by two 2100 hp Lycoming T55 engines
N.501 was a 8 passenger large version of N.500,powered by two 2650 hp Lycoming T55 turboshaft engines
N.510 was a tethered platform for use in battlefield observation,could be raise to 300m
N.511 was a version of N.510,could be raise to 1000m
N.520 was a heavy hovercraft
N.600/I was a very large transport high-wing monoplane,powered by eight turbojet engines,mounted
each four in one pod under each wing
N.600/II was a low-wing jet airliner Project,powered by four turbojet engines,mounted at the side
of the rear fuselage,one above one in each way
SN.600 Diplomate was a low-wing business jet monoplane aircraft,powered by two Pratt & Whitney Canada
JT15D-1 turbofan engines,each one mounted at the side of the rear fuselage part,developed with Sud-Aviation
SN.601 Corvette was a production version with longer fuselage than SN.600,powered by two JT15D-4 turbofan
engines,also with Sud-Aviation
SN.602 Corvette was a developed version by Aerospatiale,but powered by two Snecma Turbomeca Larzac 03 turbofan engines
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chercheuravions
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I have a little question, have we the drawing of the NC.1500 noréclair with the functionnal turret, or the drawing of the NC.1510 version?
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We have only Nord N.1500 drawing,but there is no paint to N.1510.
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Hi Stargazer,
unfortunately, this is a legend. This designation was not used. I never seen any evidence that any project was started under this designation and, for sure, no production was done.
You may remove this Nord 1102 from your list.
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In Wikipedia,there are many sources for it,and I have one of them ?.
Nord Noralpha - Wikipedia
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Yes, I know that Wikipedia has the big default to always push alive all errors published at least once.In Wikipedia,there are many sources for it,and I have one of them ?.
Nord Noralpha - Wikipedia
en.wikipedia.org
But I insist: Nord Aviation has never built any Nord 1102. You can check all photos you want, you will never found any. Bernard Chenel has established the complete production list of Nord 1100/1101/1110, and he confirmed that no Nord 1102 has been produced.
Even in the archives from Nord Aviation, I never found any mention of such designation.
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That's only my speculations about the missing numbers of the series,not
to be confuse,I suggest to complete the gaps;
Seaplane Jet Fighter N.1900 ?,1952
Mach 2 Bomber N.2300 ?, 1953/54
Ramjet powered Bomber N.2400 ?, 1955
Twin Jet Bomber N.3700 ?, 1957/59
Super Griffon N.3800 ?, 1958/60
Mach 3 N.3900 ?, 1960
Mach 4 N.4000 ?, 1960
Minerve N.4100 ?, 1960/61
Norapter N.4500 ?, 1962/63
Patrouilleur N.4600 ?, 1965
Police de l’Air Interceptor N.4700 ?, 1965
Spacecraft I & Spacecraft II N.4800 ?, 1964/1965
VTOL Vehicle I & VTOL Vehicle II N.4900 ?, 1967
VG Fighter N.7000 ?, 1970
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The SNCAN/Nord-Aviation designation system was very complicated. Internally, they used mixed designations with numbers and letters: AT, ATS, TR, E2, E3, etc. The problem is that some of these cover multiple projects, or simply internal study. So the correspondance is almost impossible to confirm.
For example, I attach some plans of the E3.
For example, I attach some plans of the E3.
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My dear Philippe,
can you display these projects in this topic,
And many thanks.
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I apologize, it's a mistake from my side: by exploring many other plans I have about SNCAN studies, I finally understood that the designation TA, TR, TM, AT, ATS, E1, E2, E3, etc. are not related to the projects, but refer to the department that provided the documents. It is not so evident on some plans, but attached example is clearer.
