Results 71 to 80 of about 38,024 (216)
Cold solid propellant motor has stop-restart capability [PDF]
, 1966 Solid propellant rocket is kept and fired at low temperatures in launch vehicles or spacecraft. The motor is capable of developing a specific impulse comparable to that of liquid propellant motors, is started, stopped, and restarted, and is stored in ...
Hendel, F. J.
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Complex Burn Region Module (CBRM) update [PDF]
Presented here is a Complex Burn Region Module (CBRM) update for the Solid Rocket Internal Ballistics Module (SRIBM) Program for the Advanced Solid Rocket Motor (ASRM) design/performance assessments.
Adams, Carl L., Jenkins, Billy
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Bond Assembly FOD Zones - A Procedure for Assuring Acceptable Adhesion [PDF]
, 2009 Rocket motor components are primarily assembled by adhesion. a) For example, the RSRM (Reusable Solid Rocket Motor - part of the Space Shuttle Boosters) system contains 10,000 sq ft of bondline area.
Evans, Kurt +2 more
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Spherical solid-propellant rocket motor Patent [PDF]
, 1961 Spherical solid propellant rocket engine ...
Styles, C. M. +2 more
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Post-impact behavior of composite solid rocket motor cases [PDF]
In recent years, composite materials have seen increasing use in advanced structural applications because of the significant weight savings they offer when compared to more traditional engineering materials.
Highsmith, Alton L.
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A survey of structural dynamics of solid propellant rocket motors [PDF]
Structural dynamics survey for solid propellant rocket ...
Baltrukonis, J. H.
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Past and Present Large Solid Rocket Motor Test Capabilities [PDF]
, 2011 A study was performed to identify the current and historical trends in the capability of solid rocket motor testing in the United States. The study focused on test positions capable of testing solid rocket motors of at least 10,000 lbf thrust.
Kowalski, Robert R., Owen, David B., II
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Kick Solid Rocket Motor Multidisciplinary Design Optimization Using Genetic Algorithm
Journal of Aerospace Technology and Management, 2013 http://dx.doi.org/10.5028/jatm.v5i3.225 In this paper, a multidisciplinary design optimization (MDO) approach of a solid propellant kick rocket motor is considered. A genetic algorithm optimization method has been used.
Fredy Marcell Villanueva +2 more
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Technologies and New Methods for Determining the Burning Rate of Solid Propellants [PDF]
فناوری در مهندسی هوافضا, 2019 The burning rate plays animportant role in determining the performanceandballistic behavior of solid rocket propellant. In this paper, the effect of various factorson burning rate, such as combustion chamber pressure, poropellant grain initial ...
Mohammad Ali Dehnavi, Reza Emami
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Performance of a UTC FW-4S solid propellant rocket motor under the command effects of simulated altitude and rotational spin [PDF]
One United Technology Center FW-4S solid-propellant rocket motor was fired at an average simulated altitude of 103,000 ft while spinning about its axial centerline at 180 rpm. The objectives of the test program were to determine motor altitude ballistic
Merryman, H. L., Smith, L. R.
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