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Powered by a booster and a sustainer solid rocket engine, the first versions could engage only subsonic targets at altitudes up to 1

...val nozzle used to produce supersonic velocity of the exhaust gases from a rocket engine.}} ...in some types of [[steam turbine]] and it is an essential part of modern [[rocket engine]]s as well as being used in supersonic [[jet engine]]s.

...Talos was launched and brought up to ramjet operating speed with a solid [[rocket engine]]. It could use a high explosive or nuclear warhead. Midcourse guidance was

A '''rocket engine''', also called '''rocket motor''', actually propels a rocket-propelled [[g At the most elementary level, the more gas a rocket engine pushes through its nozzle, and the longer the time period for which it does

...on, there were three versions of the missile. All used solid propellant [[rocket engine]]s, which were a fortuitous development of Navy-funded basic chemistry rese

...wer the new design, [[Valentin Glushko]], who then held a near-monopoly on rocket engine design in the Soviet Union, proposed a new engine, the [[RD-270]], running ...h the deliberately fuel-rich exhaust. The ring-like arrangement of so many rocket engine nozzles on the N1's first stage could have been an attempt at creating a cr

...at a fire, in a submerged submarine, was a far greater risk to the Trident rocket engine rather than the warhead. In either case, the only plausible response would

Its liquid-fueled rocket engine powered it for approximately a minute, with stabilization and some control

...es not have any type of active propulsion, either internal to it such as a rocket engine, or imparted to it externally, as by the rapid combustion of a propellant i

...ant]] ([[monomethylhydrazine]] and [[nitrogen tetroxide]]) liquid-fueled [[rocket engine]] which could be [[gimbal|gimballed]] up to 9 [[degree (angle)|degree]]s. T

...atellites have worldwide coverage, and detect intense heat sources such as rocket engine ignition.

...orifice plate]] hole, a leak in a gas pipeline or other gas container, a [[rocket engine]] exhaust nozzle, etc.</ref> into a lower pressure environment. ...icular mass flow rate. Choked flow in a [[de Laval nozzle]] as used in a [[rocket engine]] can be accelerated to [[supersonic]] linear velocities.

...total momentum of the ship plus filled fuel tank is zero. Then ignite the rocket engine and assume that its exhaust gases go one way (say downward). The exhaust ga

...ates, intensity, and spectral characteristics of a light source, such as a rocket engine, or a missile reentry vehicle. Electro-optical MASINT involves obtaining in

!Rocket engine ...[[heat exchanger]] before passing through a ramjet and/or turbojet and/or rocket engine.

# [[Rocket engine]]

#SM-3 Block II with more powerful rocket engine; available 2018

* The [[De Laval]] nozzles used in [[rocket engine]]s are essentially venturi tubes.

...bureau in 1931. By 1933, they had tested a five-ton liquid propellant [[rocket engine]], but this was not followed into long-range missile development. <ref>{{c