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Rocket

About: Rocket is a research topic. Over the lifetime, 14018 publications have been published within this topic receiving 95852 citations. The topic is also known as: rockets.


Papers
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Journal ArticleDOI
01 Aug 1969-Wear
TL;DR: In this article, a high-speed rocket sleds, traveling at velocities approaching or exceeding 6000 ft/sec have been observed to cause a gouging type of damage to the steel guiding rail of the rocket track.

30 citations

Patent
23 Oct 2003
TL;DR: In this article, the main subassemblies of a lifting system include an array of large helium-filled dirigibles, of a size that can provide hundreds or thousands of tons of lifting force; a tank-holding assembly that will be tethered to the dirigible, and that will contain pumps and high-pressure tanks, to recapture and store the helium for use in subsequent launches; and a winged platform, with wings that can be rotated vertically during liftoff, and horizontally to establish forward flight after a desired altitude has been reached, and having conventional aircraft
Abstract: A system is disclosed for lifting a rocket into the upper atmosphere and establishing forward flight at several hundred miles per hour, before the rocket engines are ignited and the rocket is released from the lifting system. The main subassemblies of this lifting system comprise: (1) an array of large helium-filled dirigibles, of a size that can provide hundreds or thousands of tons of lifting force; (2) a tank-holding assembly that will be tethered to the dirigibles, and that will contain pumps and high-pressure tanks, to recapture and store the helium for use in subsequent launches; and, (3) a winged platform, with wings that can be rotated vertically during liftoff, and horizontally to establish forward flight after a desired altitude has been reached, and having conventional aircraft engines on each wing. This system enables safer, less expensive, and more efficient launching of rockets and heavy payloads into space, using easily reusable subassemblies.

30 citations

Journal ArticleDOI
TL;DR: A survey of rocket experiments undertaken to study auroral zone events can be found in this article, which includes summary information about instrumentation and results in the field of energetic electrons and protons, of charged particle densities, of optical observations, of magnetic and electric fields, of bremsstrahlung X-rays, of thermal electrons, and of production rates.
Abstract: A survey of rocket experiments undertaken to study auroral zone events includes summary information about instrumentation and results in the field of energetic electrons and protons, of charged particle densities, of optical observations, of magnetic and electric fields, of bremsstrahlung X-rays, of thermal electrons, and of production rates. Other auroral investigations except those involving rockets have been largely ignored.

30 citations

01 Feb 1993
TL;DR: In this article, a response surface methodology for multidisciplinary optimization was used to determine the minimum dry weight entry vehicle to meet constraints on landing velocity and on subsonic, supersonic, and hypersonic trim and stability.
Abstract: A reusable rocket-powered, single-stage launch vehicle has been designed as a part of NASA's Advanced Manned Launch System (AMLS) study to examine options for a next-generation manned space transportation system. The configuration selection process utilized a response surface methodology for multidisciplinary optimization. The methodology was utilized to determine the minimum dry weight entry vehicle to meet constraints on landing velocity and on subsonic, supersonic, and hypersonic trim and stability. Once the optimum configuration was determined, a multidisciplinary conceptual vehicle design was performed. This paper presents the results of the configuration selection methodology and summarizes the overall conceptual design process with special attention given to the individual disciplines of weights/ sizing, structures/materials, configuration, flight mechanics, aerodynamics, aeroheating, propulsion, and operations.

30 citations

Journal ArticleDOI
TL;DR: In this article, a mixture of 80% polytetrafluoroethylene and 20% boron was considered as a potential high-density solid fuel mixture for mixed hybrid rocket propulsive applications.
Abstract: A composition consisting of 80% polytetrafluoroethylene and 20% boron (by weight) was considered as a potential high-density solid fuel mixture for mixed hybrid rocket propulsive applications. Constant-pressure strand burner experiments for the given formulation indicated a low-pressure self-deflagration limit of approximately 2.2 MPa (319 psia), and a burning rate correlation rb[cm/s]=0.042(P[MPa])0.531 was determined. Pressurized counterflow burner experiments conducted using pure oxygen revealed formation of surface char, which prevented measurement of solid fuel regression rates below 2 MPa, indicating an additional resistance for heat and mass transfer. Static-fired rocket motor experiments, conducted to determine the pressure and flow dependencies of the system, exhibited characteristic exhaust velocity efficiencies ranging from approximately 86 to 96%. Whereas classical hybrids do not have a strong dependence of fuel regression rate on pressure, a pressure dependence was observed in this system bel...

30 citations


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Performance
Metrics
No. of papers in the topic in previous years
YearPapers
202211
2021373
2020480
2019624
2018537
2017493