IWIS 2021 - ID168 - Missile Engine Exhaust Nozzle

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International Warsaw Invention Show IWIS 2021
Invention ID168
Title: Missile Engine Exhaust Nozzle
Short description: The invention relates to a missile control system using hybrid thrust vector control. The solution combines a pivoting nozzle and cooperating movable jet vanes. The purpose of the invention is to increase the maneuverability of the missile during each phase of flight, resulting in increased defensive capabilities and guidance accuracy.
Kielce University of Technology, Faculty of Mechatronics and Mechanical Engineering,
iwis.polskiewynalazki.pl/#/en/...

Опубликовано:

7 окт 2021

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Комментарии : 11

@memesfromtheforsakenworlwi9218 8 месяцев назад

I assure you federal agents that me looking at this right after remote detonation devices is a pure coincidence

@Gvozd111 8 месяцев назад

I wonder how the hinges hold under pressure

@amerm.m.a7154 6 месяцев назад

Hello, thank you for your good video. I want to make a small guided rocket. I wanted to know what I should do to make a guidance kit that can guide the rocket to a certain point. Do you have any training in this field? I would like to make a sample like you, of course, not with a war cap 😂 but a cap with paint inside

@tareksma1 6 месяцев назад

You can solve the problem using ardupilot or mission planner. Then u make the way point u want. The missile will follow by GPS a d you control even the altitude.

@jerohnful 7 месяцев назад

Order

@retard1582 7 месяцев назад

No way this works IRL, way more manufacturable to do it as it's been done for 30 years.

@munderabukhder9022 7 месяцев назад

Could you give me a brief explanation or a link to how it has typically been done? Fins maybe?

@a.1441 6 месяцев назад

Jet vanes have been around since the 60s at least

@shere_kan8329 5 месяцев назад

For now, missiles have been using canards and/or movable fins to control the trajectory. Newer designs include jet vanes (coupled with the fins) for thrust vectoring, see the Aim 9x (many videos on yt)