@randomradio @Rajput Lion @Parthu
I remember article by indranil roy saying Mk2 nose cone diameter will be reduced but will carry same Mk1A radar..which will decrease radar cross section & improve aircraft range like that...
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@randomradio @Rajput Lion @Parthu
I remember article by indranil roy saying Mk2 nose cone diameter will be reduced but will carry same Mk1A radar..which will decrease radar cross section & improve aircraft range like that...
Every sentence is worth a tweet..
> Mk2 endurance is 120 mins vs 57 In mk1
( Mk 2 range 3000 km with both internal & external fuel )
> Mk2 payload is 6500 kg vs 3500 kg in mk1
> MK2 manufacturing has 40 modules vs 5 in mk1. ( 25/ year production can be achieved,not sure from how many lines)
> Mk2 has internal IRST, EW vs pod in Mk1
> Mk2 has quick turnaround time
> Mk2 has health monitoring systems
Its been 6 years since this article published. Lets sink that in.
All of this was known for years now. Even the modular bit was mentioned by Saurav Jha in 2019.
Instead, for MWF, ADA is working on a modular concept in which electric looms, piping, and connectors are terminated at sub-assembly interfaces with appropriate interconnectors [18]. All the major sub-assemblies namely the three fuselage sections, wings, and the fin are also being designed with this modular approach in mind. Four Tier-1 suppliers have already been identified to take up these high-level sub-assemblies. These high level sub-assemblies are further subdivided into modular sub-sub-assemblies and so on. These, in turn which will be outsourced to Tier-2/3 suppliers. The assembly will take place using a ‘jig-less’ assembly process [3]. In this approach, the jigs are modular by design and have more versatility to adapt to any changes in the build standard of the aircraft.
View attachment 40878
All of this was known for years now. Even the modular bit was mentioned by Saurav Jha in 2019.
Instead, for MWF, ADA is working on a modular concept in which electric looms, piping, and connectors are terminated at sub-assembly interfaces with appropriate interconnectors [18]. All the major sub-assemblies namely the three fuselage sections, wings, and the fin are also being designed with this modular approach in mind. Four Tier-1 suppliers have already been identified to take up these high-level sub-assemblies. These high level sub-assemblies are further subdivided into modular sub-sub-assemblies and so on. These, in turn which will be outsourced to Tier-2/3 suppliers. The assembly will take place using a ‘jig-less’ assembly process [3]. In this approach, the jigs are modular by design and have more versatility to adapt to any changes in the build standard of the aircraft.
View attachment 40878