سهم نارى صاروخ قنبلة او قذيفة صاروخية - traduction vers Anglais
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سهم نارى صاروخ قنبلة او قذيفة صاروخية - traduction vers Anglais


سهم نارى صاروخ قنبلة او قذيفة صاروخية      

rocket (N)

rocket         
  • A balloon with a tapering nozzle. In this case, the nozzle itself does not push the balloon but is pulled by it. A convergent/divergent nozzle would be better.
  • [[Apollo 6]] while dropping the interstage ring
  • Launch of [[Apollo 15]] [[Saturn V]] rocket: ''T'' − 30 s through ''T'' + 40 s
  • boilerplate]] crew module
  • Spacecraft staging involves dropping off unnecessary parts of the rocket to reduce mass
  • 104}} during launch phase
  • Plot of instantaneous propulsive efficiency (blue) and overall efficiency for a rocket accelerating from rest (red) as percentages of the engine efficiency
  • Bumper]] sounding rocket
  • [[V-2 rocket]] launched from [[Test Stand VII]], summer of 1943
  • SRBs]], causing the breakup of the Shuttle stack
  • archive-date=2000-03-12 }}</ref>
  • Gas Core light bulb
  • Robert Goddard with a liquid oxygen-gasoline rocket (1926)
  • Rocket arrows depicted in the ''[[Huolongjing]]'': "fire arrow", "dragon-shaped arrow frame", and a "complete fire arrow"
  • Sri Lankan}} landmass
  • Illustration of the pendulum rocket fallacy. Whether the motor is mounted at the bottom (left) or top (right) of the vehicle, the thrust vector (T) points along an axis that is fixed to the vehicle (top), rather than pointing vertically (bottom) independent of vehicle attitude, which would lead the vehicle to rotate.
  • A battery of Soviet [[Katyusha rocket launchers]] fires at German forces during the [[Battle of Stalingrad]], 6 October 1942
  • Forces on a rocket in flight
  • Grossly overexpanded}}
  • Rocket thrust is caused by pressures acting on both the combustion chamber and nozzle
  • [[Mysorean rockets]] and [[rocket artillery]] used to defeat an East India Company battalion during the Battle of Guntur
  • 105}} on [[STS-134]]
  • Workers and media witness the Sound Suppression Water System test at [[Launch Pad 39A]]
  • Trident II missile]] launched from sea
  • The Tsiolkovsky rocket equation gives a relationship between the mass ratio and the final velocity in multiples of the exhaust speed
  • Viking 5C]] rocket engine
  • bombardment of Copenhagen]] (1807) during the [[Napoleonic Wars]]
PYROKINETIC ENGINE USED FOR PROPULSION; FOR THE INCENDIARY WEAPON, SEE Q2037215
Rocket launch; Rockets; Rocket launch technology; Rocket (aeronautics); Hale rocket; Rocket and missile system; Rocket and Missile System; Rocket (spacecraft); Rocket Chair; Rocket vehicle; 🚀; Rocket body; Rocket launching; Rocket blast-off; Pendulum rocket fallacy; Dogleg (rocketry); Razzo
N
الجرجير ، الكثاة (نبات يؤكل ورقه ) سهم نارى صاروخ قنبلة او قذيفة صاروخية
VT
نقل بصاروخ
I
ارتفع او انطلق كالصاروخ
السهم         
  • سهام تقليدية

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