Zilzal rocket - traduzione in Inglese
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Zilzal rocket - traduzione in Inglese

IRANIAN 610 MM HEAVY ARTILLERY ROCKET
Mushak-200; Zilzal; זילזל; Zelzal 2
  • Map with Zelzal-2 operators in blue

Zilzal rocket      
n. razzo Zilzal, razzo realizzato dall"Iran che pu? coprire una distanza di circa 200 chilometri
rocket motor         
  • Armadillo Aerospace's quad vehicle]] showing visible banding (shock diamonds) in the exhaust jet
  • Exhaust exits nozzle
}}
  • Opel RAK.1 - World's first public flight of a manned  rocket-powered plane on September 30, 1929
  • The four expansion regimes of a de Laval nozzle:
• under-expanded
• perfectly expanded
• over-expanded
• grossly over-expanded
  • Rocket vehicle mechanical efficiency as a function of vehicle instantaneous speed divided by effective exhaust speed. These percentages need to be multiplied by internal engine efficiency to get overall efficiency.
  • Rocket thrust is caused by pressures acting in the combustion chamber and nozzle. From Newton's third law, equal and opposite pressures act on the exhaust, and this accelerates it to high speeds.
  • Exhaust exits nozzle
}}
  • Viking 5C rocket engine]] used on [[Ariane 1]] through [[Ariane 4]]
NON-AIR BREATHING JET ENGINE USED TO PROPEL A MISSILE OR VEHICLE
Chemical rocket; Rocket motor; Rocket engines; Rocket engine cooling; Vacuum Isp; Hydrogen reactor; Rocket Engines; Rocket Dynamics; Rocket Engine; Throttleable rocket engine; Rocket engine throttling; Rocket engine restart; History of rocket engines; Rocket ignition; Rocket engine transients; Rocket engine ignition; Rocket-engine; Rapid Unscheduled Disassembly
motore a razzo (motore a combustione interna che utilizza la pressione prodotta dallo scoppio del"energia per spingere in avanti il corpo del razzo)
thrust chamber         
  • Figure 1: A de Laval nozzle, showing approximate flow velocity increasing from green to red in the direction of flow
  • RSA-3]] rocket
  • Diagram of a de Laval nozzle, showing flow velocity (v) increasing in the direction of flow, with decreases in temperature (t) and pressure (p). The Mach number (M) increases from subsonic, to sonic at the throat, to supersonic.
  •  grossly overexpanded.
 }}
If a nozzle is under- or overexpanded, then loss of efficiency occurs relative to an ideal nozzle.

Grossly overexpanded nozzles have improved efficiency relative to an underexpanded nozzle (though are still less efficient than a nozzle with the ideal expansion ratio), however the exhaust jet is unstable.<ref name="NASA"/>
TYPE OF PROPELLING NOZZLE
Rocket engine nozzles; Rocket nozzle; Rocket engine expansion; Thrust chamber
camera di spinta

Definizione

rocket
n.
device propelled by a rocket engine or explosives
1) to fire; launch a rocket
2) a booster; liquid-fuel; long-range; multistage; solid-fuel rocket
reprimand
(colloq.) (BE)
3) to give smb. a rocket
4) to get a rocket

Wikipedia

Zelzal-2

Zelzal-2/Mushak-200 (Persian: زلزال-۲, meaning "Earthquake") is an Iranian unguided long-range artillery rocket. The Zelzal-2 is a 610 mm truck-launched rocket that has a payload of 600 kg and a range of about 200 km. Development of the Zelzal series began in 1990 and the Zelzal-2 was first shown in 1998. It is developed from the Zelzal-1 and was developed into the Zelzal-3. It has been exported to Syria, Hezbollah, and the Houthis, and has seen combat use in the Syrian Civil War and Yemeni Civil War.

The missile is thought to be based on the Soviet 9K52 Luna-M missile.