Relevant bibliographies by topics / Solid Rocket Motors

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Solid Rocket Motors'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Solid Rocket Motors.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Solid Rocket Motors"

1

Abdelraouf, A. M., O. K. Mahmoud, and M. A. Al-Sanabawy. "Thrust termination of solid rocket motor." Journal of Physics: Conference Series 2299, no. 1 (2022): 012018. http://dx.doi.org/10.1088/1742-6596/2299/1/012018.

Full text
Abstract:
Abstract Rocket motors are engines that create the necessary thrust for the rocket motion. There are different types of rocket motors based on the propellant state, such as solid propellant rocket motors, liquid propellant rocket motors, and hybrid propellant rocket motors. One of the biggest disadvantages of solid propellant rocket motors, in comparison to liquid and hybrid propellant rocket motors, is that they are extremely difficult to extinguish, necessitating the use of specific devices. This paper reviews various ways for thrust termination such as fluid injection, rapid increase in thr
APA, Harvard, Vancouver, ISO, and other styles
2

Hu, Xiaomei, Yuting Hua, Jiahong Weng, Xianshu Teng, and Mingnan Zhang. "Performance prediction method of solid rocket motor based on the ground test." Journal of Physics: Conference Series 2816, no. 1 (2024): 012053. http://dx.doi.org/10.1088/1742-6596/2816/1/012053.

Full text
Abstract:
Abstract Solid rocket motor (SRM) is a core component of rockets. Considering the high cost of solid rocket motors and the high demand for transportation and storage, there is an urgent need to predict the performance of solid rocket motors before the ground ignition test to lower the cost of tests. Using data mining technology to predict various parameters of rocket motors with historical data has become a new development direction. In order to improve the data fitting effect and prediction accuracy, a novel prediction model was proposed, which tries to combine the Whale Optimization Algorith
APA, Harvard, Vancouver, ISO, and other styles
3

Schonberg, W. P. "Energy partitioning in high speed impact of analogue solid rocket motors." Aeronautical Journal 103, no. 1029 (1999): 519–28. http://dx.doi.org/10.1017/s0001924000064277.

Full text
Abstract:
Abstract Modelling the response of solid rocket motors to bullet and fragment impacts is a high priority among the military services from standpoints of both safety and mission effectiveness. Considerable effort is being devoted to characterising the bullet and fragment vulnerability of solid rocket motors, and to developing solid rocket motor case technologies for preventing or lessening the violent responses of rocket motors to these impact loadings. Because full-scale tests are costly, fast-running analytical methods are required to characterise the response of solid rocket motors to ballis
APA, Harvard, Vancouver, ISO, and other styles
4

Kessler, D. J. "Explorer 46 Meteoroid Bumper Experiment: Earth Orbital Debris Interpretation." International Astronomical Union Colloquium 85 (1985): 97. http://dx.doi.org/10.1017/s0252921100084414.

Full text
Abstract:
AbstractThe Meteoroid Bumper Experiment on Explorer 46 (launched 1972) was placed in Earth orbit to evaluate the effectiveness of using double-wall structures against meteoroids. This paper re-examines the data from this experiment. Certain sets of sensors were found to be penetrated much more frequently than other sets. The most plausible explanation is that nearly all of the penetrations were from an Earth orbiting population of particulates. In addition, because a large percentage of the penetrations occured soon after solid rocket motors were fired in space, the particulates are most likel
APA, Harvard, Vancouver, ISO, and other styles
5

Said, A., A. Maraden, T. M. Elhedery, A. M. abd Elall, and S. Elbasuney. "Propulsion theoretical and experimental analysis of composite propellants motors." Journal of Physics: Conference Series 2616, no. 1 (2023): 012057. http://dx.doi.org/10.1088/1742-6596/2616/1/012057.

Full text
Abstract:
Abstract Rockets have revolutionized space technology and human space exploration. Most rockets and missiles are both propelled by rocket motors that use composite solid propellants. The ICT code and the NSAS CEA code are two programs that can be used to forecast theoretical propulsion parameters for composite solid rocket propellant. Rocket propellant performance is governed by a specific impulse factor, which is calculated theoretical and experiment. In this paper, the theoretical specific impulse for different composite solid propellant formulations at 70 bar combustion pressure and an adap
APA, Harvard, Vancouver, ISO, and other styles
6

Mihailescu, Cristina. "Practical Methods of Optimizing the Maximum Range for Rockets." International Journal on Applied Physics and Engineering 2 (October 5, 2023): 137–43. http://dx.doi.org/10.37394/232030.2023.2.13.

Full text
Abstract:
Range extension for artillery projectiles, rockets, and missiles is a problem of trajectory optimization based on a set of constraints aimed at maximizing the range as a measure of performance. Solid Rocket Motors (SRM) are rocket motors that use solid propellants. For higher engine efficiency and cost minimization, optimization of the engine is necessary, which implies a modification of the schematics of the engine. SRM optimization is currently a key topic in aerospace engineering research. Because some input data remain constant, others can be considered as variables, and their influence on
APA, Harvard, Vancouver, ISO, and other styles
7

Jadhav, Shruti Dipak, Tapas Kumar Nag, Atri Bandyopadhyay, and Raghvendra Pratap Singh. "Experimental and Computational Investigation of Sounding Solid Rocket Motor." 3 1, no. 3 (2022): 29–38. http://dx.doi.org/10.46632/jame/1/3/5.

Full text
Abstract:
Experimental sounding rockets are important contributors to aerospace engineering research. However, experimental-sounding rockets are rarely used for student research projects by institutes in India. The unavailability of rocket motors, which require complex machining and explosive propellants, is a major barrier to the use of sounding rockets in student research projects. We ran into this problem while developing a sounding rocket motor for project and learning purposes. The project focuses on designing and constructing a solid rocket motor that researchers can use as the primary propulsion
APA, Harvard, Vancouver, ISO, and other styles
8

Nagappa, R., M. R. Kurup, and A. E. Muthunayagam. "ISRO's solid rocket motors." Acta Astronautica 19, no. 8 (1989): 681–97. http://dx.doi.org/10.1016/0094-5765(89)90136-7.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Serrano, Dario Donrey. "Applications of Optimization Techniques for Solid Rocket Design." Highlights in Science, Engineering and Technology 38 (March 16, 2023): 716–24. http://dx.doi.org/10.54097/hset.v38i.5936.

Full text
Abstract:
Solid Rocket Motors (SRM) are rocket motors that use solid propellants (fuel/oxidizer). Optimization of the motor’s design is the process to alter the schematics of the engine for higher engine efficiency and cost minimization. Solid Rocket Motor optimization is one of the key topics of aerospace engineering research today. Conventional methods for optimization have fallen obsolete due to the exceedingly large number of design variable in modern rocket engine optimization. This paper will summarize and review some of the related research carried out in this field. Modern methods of optimizatio
APA, Harvard, Vancouver, ISO, and other styles
10

Zhang, Yin, Zhensheng Sun, Yu Hu, et al. "Numerical Simulation of the Gas Flow of Combustion Products from Ignition in a Solid Rocket Motor Under Conditions of Propellant Creep." Aerospace 12, no. 2 (2025): 153. https://doi.org/10.3390/aerospace12020153.

Full text
Abstract:
The development of modern solid rocket technology with high-performance and high-loading ratio propellants places higher requirements on the safety and stability of the solid rocket motor. The propellant of the solid rocket motor will creep during long-term vertical storage, which may adversely affect its regular operation. The ignition transient process is a critical phase in the operation of solid rocket motors. The Abaqus v.2022 finite element simulation software is used to analyze the ignition transient under propellant creep conditions and obtain the deformed combustion chamber profile. T
APA, Harvard, Vancouver, ISO, and other styles
More sources

Dissertations / Theses on the topic "Solid Rocket Motors"

1

Hovland, Douglas Lyle. "Particle sizing in solid rocket motors." Thesis, Monterey, California. Naval Postgraduate School, 1989. http://hdl.handle.net/10945/26153.

Full text
Abstract:
Particle size distribution measurements were made with a Malvern 2600c forward laser light diffraction system across the exhaust nozzle entrance and exhaust plume of a small two-dimensional rocket motor. The solid propellants tested were GAP propellants containing 2.0% and 4.69% aluminum. Surface agglomeration of the aluminum, indicated by the in-motor results, was found to decrease as the motor chamber pressures were increased. At low pressures, increasing the aluminum loading with fixed total solids decreased the mean particle size at the nozzle entrance. Exhaust plume particle size was prac
APA, Harvard, Vancouver, ISO, and other styles
2

McCrorie, J. David. "Particle behavior in solid propellant rocket motors and plumes." Thesis, Monterey, California. Naval Postgraduate School, 1992. http://hdl.handle.net/10945/24002.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Puskulcu, Gokay. "Analysis Of 3-d Grain Burnback Of Solid Propellant Rocket Motors And Verification With Rocket Motor Tests." Master's thesis, METU, 2004. http://etd.lib.metu.edu.tr/upload/12605270/index.pdf.

Full text
Abstract:
Solid propellant rocket motors are the most widely used propulsion systems for military applications that require high thrust to weight ratio for relatively short time intervals. Very wide range of magnitude and duration of the thrust can be obtained from solid propellant rocket motors by making some small changes at the design of the rocket motor. The most effective of these design criteria is the geometry of the solid propellant grain. So the most important step in designing the solid propellant rocket motor is determination of the geometry of the solid propellant grain. The performance p
APA, Harvard, Vancouver, ISO, and other styles
4

Matta, Lawrence Mark. "Investigation of the flow turning loss in unstable solid propellant rocket motors." Diss., Georgia Institute of Technology, 1993. http://hdl.handle.net/1853/15938.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Romano, Federico. "Q1D unsteady ballistic model for solid rocket motors performance prediction." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2021.

Find full text
Abstract:
The simulation tool ROBOOST, in use at the Alma Propulsion Lab of the University of Bologna – Forlì Campus, exploits a hybrid ballistic model 0D-1D. The need of a complete Q1D model for the entire combustion time, from motor start-up to burn out arised. The present work is devoted to the development and test of a Q1D unsteady ballistic model for solid rocket motors performance prediction. The newly developed code, called SOL1D, is written in Matlab environment and is capable of predicting the time and space evolution of all the main thermodynamic variables during the solid rocket motor combust
APA, Harvard, Vancouver, ISO, and other styles
6

Yakin, Bülent. "Combustor and nozzle effects on particulate behavior in solid rocket motors /." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1993. http://handle.dtic.mil/100.2/ADA277304.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Yakin, Bulent. "Combustor and nozzle effects on particulate behavior in solid rocket motors." Thesis, Monterey, California. Naval Postgraduate School, 1993. http://hdl.handle.net/10945/39764.

Full text
Abstract:
Approved for public release; distribution is unlimited.<br>An investigation was conducted using a subscale solid rocket motor to measure the effect of nozzle residence time on the behavior of Al203 particles to assess the applicability of subscale motor data to full-scale motors and to measure the effects of nozzle entrance particle size distribution on the slag accumulated with submerged nozzles. Although particles as large as 140 micrometers were present at the nozzle entrance, most of the particulate mass was contained in much smaller particles. This observation is in good agreement with th
APA, Harvard, Vancouver, ISO, and other styles
8

Mini, Stefano <1991&gt. "Analysis of the main phenomena affecting solid rocket motors internal ballistics." Doctoral thesis, Alma Mater Studiorum - Università di Bologna, 2021. http://amsdottorato.unibo.it/9878/1/PhD_Thesis.pdf.

Full text
Abstract:
In solid rocket motors, the absence of combustion controllability and the large amount of financial resources involved in full-scale firing tests, increase the importance of numerical simulations in order to asses stringent mission thrust requirements and evaluate the influence of thrust chamber phenomena affecting the grain combustion. Among those phenomena, grain local defects (propellant casting inclusions and debondings), combustion heat accumulation involving pressure peaks (Friedman Curl effect), and case-insulating thermal protection material ablation affect thrust prediction in terms o
APA, Harvard, Vancouver, ISO, and other styles
9

Hasanoglu, Mehmet Sinan. "Storage Reliability Analysis Of Solid Rocket Propellants." Master's thesis, METU, 2008. http://etd.lib.metu.edu.tr/upload/2/12609897/index.pdf.

Full text
Abstract:
Solid propellant rocket motor is the primary propulsion technology used for short and medium range missiles. It is also commonly used as boost motor in many di_erent applications. Its wide spread usage gives rise to diversity of environments in which it is handled and stored. Ability to predict the storage life of solid propellants plays an important role in the design and selection of correct protective environments. In this study a methodology for the prediction of solid propellant storage life using cumulative damage concepts is introduced. Finite element mesh of the solid propellant grain
APA, Harvard, Vancouver, ISO, and other styles
10

Vernacchia, Matthew T. "Development of low-thrust solid rocket motors for small, fast aircraft propulsion." Thesis, Massachusetts Institute of Technology, 2020. https://hdl.handle.net/1721.1/127069.

Full text
Abstract:
Thesis: Ph. D., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, May, 2020<br>Cataloged from the official PDF of thesis.<br>Includes bibliographical references (pages 281-289).<br>Small, uncrewed aerial vehicles (UAVs) are expanding the capabilities of aircraft systems. However, a gap exists in the size and capability of aircraft: no small aircraft are capable of sustained fast flight. A small, fast aircraft requires a propulsion system which is both miniature and high-power, requirements which current UAV propulsion technologies do not meet. Solid propellant
APA, Harvard, Vancouver, ISO, and other styles
More sources

Books on the topic "Solid Rocket Motors"

1

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Design methods in solid rocket motors. AGARD, 1988.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
2

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Design Methods in Solid Rocket Motors. s.n, 1987.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
3

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. and North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Consultant and Exchange Programme., eds. Design methods in solid rocket motors. North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1987.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
4

Hovland, Douglas Lyle. Particle sizing in solid rocket motors. Naval Postgraduate School, 1989.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
5

Langhenry, M. T. Acceleration effects in solid propellant rocket motors. AIAA, 1986.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
6

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

L, Derr Ronald, and North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., eds. Hazard studies for solid propellant rocket motors. AGARD, 1990.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
8

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hazard studies for solid propellant rocket motors. AGARD, 1990.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
9

McCrorie, J. David. Particle behavior in solid propellant rocket motors and plumes. Naval Postgraduate School, 1992.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
10

Greatrix, David R. A study of combustion and flow behaviour in solid-propellant rocket motors. [Institute for Aerospace Studies], 1987.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Book chapters on the topic "Solid Rocket Motors"

1

Greatrix, David R. "Solid-Propellant Rocket Motors." In Powered Flight. Springer London, 2012. http://dx.doi.org/10.1007/978-1-4471-2485-6_10.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. "Erosion Characteristics of Fluidic Throat in Solid-Rocket Motors." In Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6_8.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. "Thrust Modulation Process of Fluidic Throat for Solid Rocket Motors." In Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6_7.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. "Introduction." In Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6_1.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. "System Application Modes and Key Technologies." In Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6_10.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. "Steady Characteristics of a Gas–Gas Aerodynamic Throat." In Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6_2.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. "The Characteristic Function and Nozzle Efficiency." In Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6_3.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. "The Fluidic Throat in Gas–Particle Two-Phase Flow Conditions." In Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6_4.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. "Secondary Flow TVC for Fluidic-Throat Nozzles." In Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6_5.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Xie, Kan, Xinmin Chen, Junwei Li, and Yu Liu. "Gas–Liquid Fluidic Throat." In Fluidic Nozzle Throats in Solid Rocket Motors. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6439-6_6.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Solid Rocket Motors"

1

DELANNOY, GUY. "Computation of performance for different solid rocket motors - Conventional motors, nozzleless rocket motors, rocket ramjets." In 24th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3046.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

MACBETH, A. "Refurbishment of the Space Shuttle redesigned solid rocket motors - The first reusable solid rocket motors." In 25th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2403.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Courta, A. "Vortex shedding in solid rocket motors." In 33rd Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-727.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Parsons, I., P. Alavilli, A. Namazifard, A. Acharya, X. Jiao, and R. Fiedler. "Coupled simulations of solid rocket motors." In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-3456.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Guery, J., F. Godfroy, S. Ballereau, et al. "Thrust Oscillations in Solid Rocket Motors." In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-4979.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

GAUNT, D. "Understanding costs of solid rocket motors." In 22nd Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1638.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Goyal, Vinay, Jacob Rome, and Patrick Schubel. "Structural Analysis of Solid Rocket Motors." In 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
16th AIAA/ASME/AHS Adaptive Structures Conference
10t. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-2110.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Gallier, Stany, Emmanuel Radenac, and Franck Godfroy. "Thermoacoustic Instabilities in Solid Rocket Motors." In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-5252.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

HILBING, J., and S. HEISTER. "Radial slot flows in solid rocket motors." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2309.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Zgheib, Nadim, and Joseph Majdalani. "Axial Waves in Simulated Solid Rocket Motors." In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-6993.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Reports on the topic "Solid Rocket Motors"

1

Lhota, J. R., G. C. Panos, E. C. Johnson, and M. C. Gregory. Ultrasonic Backscatter Technique for Corrosion Detection in Solid Rocket Motors. Defense Technical Information Center, 1994. http://dx.doi.org/10.21236/ada307597.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

NAVAL WEAPONS CENTER CHINA LAKE CA. Measured Temperatures of Solid Rocket Motors Dump Stored in the Tropics and Desert. Part 4. Tropics. Defense Technical Information Center, 1989. http://dx.doi.org/10.21236/ada213425.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Ko, Malcolm, Run-Lie Shia, Debra Weisenstein, Jose Rodriguez, and Nien-Dak Sze. Global Stratospheric Impact of Solid Rocket Motor Launchers. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada413823.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Chelner, Herbert. Embedded Sensor Technology for Solid Rocket Motor Health Monitoring. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada405070.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Chelner, Herbert. Embedded Sensor Technology for Solid Rocket Motor Health Monitoring. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada412607.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Reaugh, J., E. Lee, and J. Maienschein. The Production of Airblast From Solid Rocket Motor Fallbacks. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1053686.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Aguilo Valentin, Miguel Alejandro, Steven W. Bova, and David R. Noble. Solid Rocket Motor Design using a Low-Dimensional Fluid Model. Office of Scientific and Technical Information (OSTI), 2019. http://dx.doi.org/10.2172/1496883.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Hyde, R. S. A Solid Rocket Motor Manufacturer's View of Sensors and Aging Surveillance. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada406078.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Koo, J. H., O. A. Ezekoye, M. C. Bruns, and J. C. Lee. Experimental and Numerical Characterization of Polymer Nanocomposites for Solid Rocket Motor Internal Insulation. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada564427.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Koo, J. H., and O. D. Ezekoye. Experimental and Numerical Characterization of Polymer Nanocomposites for Solid Rocket Motor Internal Insulation. Defense Technical Information Center, 2006. http://dx.doi.org/10.21236/ada589776.

Full text
APA, Harvard, Vancouver, ISO, and other styles
You might also be interested in the extended bibliographies on the topic 'Solid Rocket Motors' for particular source types:
Journal articles Dissertations / Theses Books
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography