ASTRA MK-2 vs METEOR | Astra Mk-2 Configuration Final | 51 Tejas mk-1a with UTTAM AESA
The Ducted Rocket (DR)
Principle :
A "gas" generator is providing the fuel species which are injected in the ramjet combustion chamber (GFRJ)
The "gas" generator is working like a solid-propellant rocket, except that the solid propellant has a low oxidizer content
The "gas" generator products can contain a high fraction of fuel particles (Mg, Al, B, C) to enhance the performances
The first operational missile using such a concept has been the Russian SA6 Gainful (Mg). Work began in France at ONERA around 1972 (A. Moutet) and related propellant activity was shared quickly with SNPE ("aerosols")
A large variety of composite propellants for DR is now available for missiles applications, for instance :
propellants for "low" IR signature missiles ("aérolite")
high density, high-performance propellants ("aérofluolèbe")
propellants for VFDR and UFDR C
ombustion mechanisms are conventional one-phase or two-phase ones===================================================
WHOMSOEVER IT MAY CONCERN
Most of the pictures clip or BGM included in the Video Belongs to their Respected Owners and we do not claim rights...but under this👇 we are using them 🙏
===================================================
DISCLAIMER: UNDER SECTION 107 OF THE COPYRIGHT ACT 1976, ALLOWANCE IS MADE FOR "FAIR USE" FOR PURPOSES SUCH AS CRITICISM, COMMENT, NEWS REPORTING, TEACHING, SCHOLARSHIP, AND RESEARCH. FAIR USE IS A USE PERMITTED BY COPYRIGHT STATUTE THAT MIGHT OTHERWISE BE INFRINGING. NON-PROFIT, EDUCATIONAL OR PERSONAL USE TIPS THE BALANCE IN FAVOR OF FAIR USE.
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SOURCE► #DefenceDecode
====================================================
THANKS FOR WATCHING,
PLEASE LIKE SHARE AND SUBSCRIBE TO THE DEFENCE DECODE
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Видео ASTRA MK-2 vs METEOR | Astra Mk-2 Configuration Final | 51 Tejas mk-1a with UTTAM AESA канала Defence Decode
Principle :
A "gas" generator is providing the fuel species which are injected in the ramjet combustion chamber (GFRJ)
The "gas" generator is working like a solid-propellant rocket, except that the solid propellant has a low oxidizer content
The "gas" generator products can contain a high fraction of fuel particles (Mg, Al, B, C) to enhance the performances
The first operational missile using such a concept has been the Russian SA6 Gainful (Mg). Work began in France at ONERA around 1972 (A. Moutet) and related propellant activity was shared quickly with SNPE ("aerosols")
A large variety of composite propellants for DR is now available for missiles applications, for instance :
propellants for "low" IR signature missiles ("aérolite")
high density, high-performance propellants ("aérofluolèbe")
propellants for VFDR and UFDR C
ombustion mechanisms are conventional one-phase or two-phase ones===================================================
WHOMSOEVER IT MAY CONCERN
Most of the pictures clip or BGM included in the Video Belongs to their Respected Owners and we do not claim rights...but under this👇 we are using them 🙏
===================================================
DISCLAIMER: UNDER SECTION 107 OF THE COPYRIGHT ACT 1976, ALLOWANCE IS MADE FOR "FAIR USE" FOR PURPOSES SUCH AS CRITICISM, COMMENT, NEWS REPORTING, TEACHING, SCHOLARSHIP, AND RESEARCH. FAIR USE IS A USE PERMITTED BY COPYRIGHT STATUTE THAT MIGHT OTHERWISE BE INFRINGING. NON-PROFIT, EDUCATIONAL OR PERSONAL USE TIPS THE BALANCE IN FAVOR OF FAIR USE.
Facebook ► https://www.facebook.com/indiatubedesk
Twitter ► https://twitter.com/indiatubedesk
ˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍˍ
SOURCE► #DefenceDecode
====================================================
THANKS FOR WATCHING,
PLEASE LIKE SHARE AND SUBSCRIBE TO THE DEFENCE DECODE
====================================================
Видео ASTRA MK-2 vs METEOR | Astra Mk-2 Configuration Final | 51 Tejas mk-1a with UTTAM AESA канала Defence Decode
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