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THE NEXT GENERATION ROCKET ENGINES
Acta Astronautica, 1989Abstract This paper examines propulsion system technologies for earth-to-orbit vehicles, and describes several propulsion system concepts which could support the recommendations of the Commission for Space Development for the year 2000. The hallmark of that system must and will be reliability.
Rudi Beichel +2 more
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Naval Engineers Journal, 1968
The rocket owes its development almost entirely to warfare and has indeed been the principal rival of the gun since the invention of powder. Unlike the gun, however, it has peaceful uses as the simplest form of prime mover. Its potential for space transport became a reality only with the invention of liquid fuel systems but more recent trends have been
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The rocket owes its development almost entirely to warfare and has indeed been the principal rival of the gun since the invention of powder. Unlike the gun, however, it has peaceful uses as the simplest form of prime mover. Its potential for space transport became a reality only with the invention of liquid fuel systems but more recent trends have been
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The Journal of the Royal Aeronautical Society, 1957
The 1,000th Lecture to be given before the Society and the 27th Main Lecture to be held at a Branch of the Society was held under the auspices of the Henlow Branch. The lecture, “Rocket Engines,” was given by Mr. S. Allen, F.R.Ae.S., on 11th October 1956. Professor A. J. Murphy, A.F.R.Ae.S., President of the Henlow Branch, opened the meeting, and Mr. E.
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The 1,000th Lecture to be given before the Society and the 27th Main Lecture to be held at a Branch of the Society was held under the auspices of the Henlow Branch. The lecture, “Rocket Engines,” was given by Mr. S. Allen, F.R.Ae.S., on 11th October 1956. Professor A. J. Murphy, A.F.R.Ae.S., President of the Henlow Branch, opened the meeting, and Mr. E.
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Cryogenic rocket engine development at Delft aerospace rocket engineering
2016Space Systems ...
Wink, J (author) +8 more
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Gas-core nuclear rocket engine
2nd Propulsion Joint Specialist Conference, 1966The major components of a gas-core nuclear rocket engine are studied, on the assumption of satisfactory hydrodynamic containment of the core. The core cavity was assumed to have a diameter and length of 60 in., a hydrogen cavity temperature of 12,000°R, a hydrogen flow rate of 200 Ib/sec, and a chamber pressure of 10,000 psia.
EDWARD E. DUKE, WILLIAM J. HOUGHTON
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Journal of Jet Propulsion, 1954
Theoretically only one type exists; however, due to the selective process of dynamic evolution, four types are known to exist at various rocket establishments. The IDEAL type is the rocket test engineer you see in the movies, ads, and press releases. He is usually clad in protective clothing, wears a face shield, and sometimes sports a supersonic dunce
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Theoretically only one type exists; however, due to the selective process of dynamic evolution, four types are known to exist at various rocket establishments. The IDEAL type is the rocket test engineer you see in the movies, ads, and press releases. He is usually clad in protective clothing, wears a face shield, and sometimes sports a supersonic dunce
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2012
The hybrid rocket engine utilizes a combination of solid rocket and liquid rocket technology to meet some flight mission applications. In terms of performance, cost, availability of materials and safety, the hybrid approach does potentially have some advantages.
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The hybrid rocket engine utilizes a combination of solid rocket and liquid rocket technology to meet some flight mission applications. In terms of performance, cost, availability of materials and safety, the hybrid approach does potentially have some advantages.
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Experimental investigation on pulse operation characteristics of rotating detonation rocket engine
Fuel, 2023Shengbing Zhou, Ning Hu
exaly