Foreign involvement in the NAL Saras Mk2
High AoA stability, Ground Effect, Single Engine Control, significant modifications of Saras Mk1: TsAGI Russia
Wind tunnel testing of Saras Mk2: Calapan Corp, USA
Cabin Design of Saras Mk2: GDC Engineering, UK
Wind tunnel testing and data generation of Saras Mk2: TsAGI, Russia
Further wind tunnel testing and data generation for Saras Mk2: ONERA, France
Nacelle design of tractor config Saras Mk2: The Nacelle Group, Northern Ireland
Seating system of Saras Mk2: Expliseat, France
Propeller for Saras Mk2: Hartzell, USA
Configuration studies for Saras Mk2: DAR Corporation, USA
Miscellaneous consultancy for Saras Mk2: Dassault Systems India Pvt. Ltd, Gurgaon
Lithium Iron Phosphate battery for Saras Mk2: Mid-Continent Instument, Kansas, USA
Windshield transparency consultancy for Saras Mk2: PPG Industries, Dubai
Hydraulic system, Flight controls, Fuel system, Electrical system, Fire protection system, other LRUs of Saras Mk2: Collins Aerospace
Design for certification of Saras Mk2: Safran Electronics and Defence, France
Landing gear system, and hydraulic LRUs: APPH Limited, UK
Engine mount isolater: Hutchinson Aerospace, USA
Brake manifold, braking system, aircraft systems related: Moog, USA and UK
Design and manufacturing of Pilot/Copilot seats: IPECO Holdings, UK
Further windshield transparency work: MECAPLEX, Switzerland
Testing of corrosion prevention primer: Hexigone Inhibitors, UK
Optimization of configuration studies: Professor Leonardo Manfriani, Switzerland
Deicing system: Goodrich Aerospace, Ohio, USA
Yoke: Crouzet, France
In the middle of writing I have forgotten to put Saras Mk2 after each of these listings... these are all for Saras Mk2.
This is what happens when you have a 1000 persons strong lab trying to be NASA, Embraer, and GE all together while having 1/250th of the budget
Next:

Above is the Sectional Velocity and Surface Cp Distribution with Flaps 15°
Aircraft 2.5m above Ground
NAL Saras Mk2
Ground effect studies show that the plane is safe for very low altitude operations, assisted by TsAGI Russia.
This was an issue that the Mk1 had issues with, when it would go into ground effect, the plane would balloon up, causing issues to handling during landing for the pilot.
It was fixed by TsAGI for both Mk1's 2018 prototype and Mk2's design...
Myasischev Design Bureau's chief designer Dr Alexander Bruk, his deputy Dr Alexander Arkhipov, Chief Specialist on Flight Dynamics Dr Eduard Abramenko, Engineer Designer on Control System Dr Vladimir Vinogadov and Dr Victor Frolovskiy from the Department of Design had come to NAL in 2010 for initiation of assistance in Saras program