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Post Info TOPIC: SNCASE / Sud-Est Aviation designation (SE-)


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SNCASE / Sud-Est Aviation designation (SE-)
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http://www.secretprojects.co.uk/forum/index.php/topic,9739.0.html



-- Edited by Stingray on Thursday 21st of April 2011 01:36:06 AM

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Date: Apr 20, 2011
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airfoil, I know you meant well, but...

It's not a good idea to duplicate my lists here as they will be evolving constantly. New stuff has already been added since you posted these.
I try my best to get all that information in one place to avoid duplications and trouble with Google caching old page versions... By creating these topics you will only add to the confusion... So please remove the contents of these posts and simply add a link to the Secret Projects topics instead.

Or I can ask Travis to do it if it's too complicated.

Thanks.

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Stéphane



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Edited your posts, Darrell.



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Hi,

 

here is an info about X-310;

Mr. Pierre Renoux designed before leaving the SNACSE company,a seven helicopter projects,
they are X-310A,B,C,D,E,F and G,the X-310G equipped with a turbine Atrouste engine,and
redesigned as SE.3130.

http://fr.wikipedia.org/wiki/Alouette_II

Also an info about X-316;

X-316 was a twenty three seat commercial and military transport helicopter project of 1955.



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hesham


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Hi,


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-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

- any additions or corrections are welcome



-- Edited by hesham on Wednesday 15th of April 2020 03:20:31 PM



-- Edited by hesham on Wednesday 15th of April 2020 03:21:29 PM

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hesham


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From post war,SNCASE used a 300 series for helicopter ;-

X-300 to X-309 were unknown designs
X-310A,B,C,D,E & F were a lightweight helicopter Projects,powered by one turboshaft engine
X-310G was a lightweight helicopter,powered by one 530 hp Turbomeca Artouste IIC6 turboshaft engine,later
developed into SE-3130 Alouette
X-311 Helibus was a tandem main rotor medium transport helicopter Project,could accommodated 30 passenger,powered by two 400 Turbomeca turbine engines
X-312,X-313 & X-314 were unknown designs

X-315 was a seven-seat utility and light flying crane helicopter Project,with single rotor and

powered by two turbine engines
X-316 was a twenty three seat commercial and military transport helicopter Project of 1955,led to develop
SE-3200 Frelon
X-3XX was a large flaying crane helicopter Project,with a payload 16.000-24.000 1b,and designed in co-operated
with Agusta and a company from Germany,1959



-- Edited by hesham on Wednesday 22nd of April 2020 07:31:43 AM



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hesham


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Date: April 17th
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hesham wrote:

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


 AKA the Alouette IV, that was its original name under the Sud Aviation heading.



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OK Leela,

and I add X-315.



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hesham
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