error 8m - in vacuum

Simulation of launching a Fath missile from an aircraft with initial velocity of mach 1 with altitude of 10 km and with two different angles in the boost phase. aircraft initial elevation angle is zero degrees. the characteristics and aerodynamic properties of the missile are vague and inaccurate. (photo: Preliminary launch test of Fajr rocket from Fitter).🚀

simulation file (KMZ) link for display in Google Earth 🌎

https://news.1rj.ru/str/Exciton_missile_program/15

@Exciton_missile_program🚀

photos are decorative.

@Exciton_missile_program 🚀

The red line is the boost phase time. the blue line is on the longer path of the terminal phase. and you see a slight deviation due to the quasi-force of coriolis, which is actually caused by the rotation of the earth and reveals itself better in the longer path.

2 مقاله خوب در رابطه با پیشرانش ژل پایه مزیتها و نقطه ضعفها. لینک آخر در رابطه با حرکت استارت آپ اسرائیلی به سمت سوختهای ژله‌ای به جهت مزیتهای آن. طبعا مسائلی مثل اسپاترینگ درست از جمله مسائلی است که باید حل شود. شناخت از میزان گرانروی نسبت به تنشهای برشی وارده به ماده. 🚀🔥

http://www.military.ir/forums/topic/30241-%D9%BE%DB%8C%D8%B4%D8%B1%D8%A7%D9%86%D8%B4-%DA%98%D9%84-%D9%BE%D8%A7%DB%8C%D9%87/

https://jangaavaran.ir/%D8%B3%D9%88%D8%AE%D8%AA-%D9%87%D8%A7%DB%8C-%DA%98%D9%84/

https://www.timesofisrael.com/startup-unveils-new-generation-rocket-engines-with-powergel-fuel/