liquid-propellant rocket technical
liquid rocket technical

This cooling design became the basis of all modern liquid-propellant rocket motors.

The propulsion for the aircraft was a liquid-propellant rocket designed by the Walter company.

The Iraqis simply strapped liquid-propellant rockets to the sides.

Developed solid and liquid-propellant rockets, with first successful flight with liquid in 1926.

The missile, which went by a variety of names depending on the version, used a single liquid-propellant rocket motor.

Liquid-propellant rockets use one or more liquid propellants fed from tanks.

The F-1 remains the most powerful single-combustion chamber liquid-propellant rocket engine ever developed.

Liquid-propellant rocket development has always proceeded in three steps:

Stage 1 used an LR87 liquid-propellant rocket engine.

The RS-27 is a liquid-propellant rocket engine developed by Rocketdyne.

For liquid-propellant rockets four different ways of powering the injection of the propellant into the chamber are in common use.

The highest specific impulse chemical rockets (liquid-propellant rockets) use liquid fuel propellants.

Revealed in 2015, the Blue Origin orbital launch vehicle is a two-stage-to-orbit liquid-propellant rocket.

A liquid-propellant rocket engine powered the second stage (modified Vanguard second stage, thrust about 7500 pounds).

Early flights used two Reaction Motors XLR11 liquid-propellant rocket engines.

The XLR99 engine was the first large, throttleable, restartable liquid-propellant rocket engine.

Goddard hesitated to discuss any of his research, other than that which had already been published in Liquid-Propellant Rocket Development.

Bongbong was a Philippine liquid-propellant rocket developed under Project Santa Barbara.

All rockets used some form of solid or powdered propellant up until the 20th century, when liquid-propellant rockets offered more efficient and controllable alternatives.

A liquid-propellant rocket or liquid rocket is a rocket engine that uses liquid propellants.

However, liquid-propellant rockets can be throttled by means of valves which regulate the flow of fuel and oxidizer to the combustion chamber.

Spacecraft propulsion (Liquid-propellant rocket)

Rockets are generally of the solid fuel type for ease of maintenance and fast deployment, although some larger ballistic missiles use Liquid-propellant rockets.

After World War II the American government and military finally seriously considered liquid-propellant rockets as weapons and began to fund work on them.

This concept is also composed of two liquid rocket stages.

The letters indicate that these concepts will have two liquid rocket stages.

The Rocketdyne division developed a variety of liquid rocket engines.

It is a common liquid rocket fuel for rocket applications.

It is the first liquid rocket engine designed in Russia after the Soviet period.

This is especially true for liquid rocket engines.

Thus it will inherit the 3.35m-diameter core stage and 2.25m-diameter liquid rocket boosters.

Apart from the space shuttle main engine, the United States developed no new power plants for liquid rockets after the 1960's.

Paulet described laboratory tests of, but did not claim to have launched a liquid rocket.

Melange is a highly toxic liquid rocket fuel component used during the Soviet era.

Most of of those companies make liquid rockets for the civilian or military rocket fleets.

Current blue-sky planning for Mars exploration assumes that we will use liquid rockets and take about a year each way.

Just as it hit the ground, the single-stage liquid rocket propellant ignited.

Liquid rocket boosters generally cannot be moved after tanking.

The Russians had gotten ahead of us in liquid rocket propulsion systems and were using simpler, more efficient designs.

Liquid rocket propulsion systems containing any of the systems or components controlled by 1091.6.

The second used liquid rocket motors and was planned to have orbited 200 pounds of payload.

C-201W: Fitted with a turbojet engine instead of a liquid rocket version.

These two substances are both non-toxic and easily stored, making them safer than liquid rocket fuels.

Systems and components specially designed for liquid rocket propulsion systems, as follows: a.

Non-storable liquid rockets require considerable preparation immediately before launch.

Thrust vectoring for many liquid rockets is achieved by gimbaling the rocket engine.

He managed the propulsion and combustion products department where he was responsible for liquid rocket engine development.

Perchloryl fluoride was investigated as a high performance liquid rocket fuel oxidizer.

It is estimated that global ozone depletion results from a mixture of solid and liquid rocket fuel emissions.