000 02330 a2200253 4500
003 OSt
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008 190912b xxu||||| |||| 00| 0 eng d
020 _a9781108422277
040 _cIIT Kanpur
041 _aeng
082 _a621.4356
_bR591
245 _aRocket propulsion
_cStephen D. Heister ...[et al.]
260 _bCambridge University Press
_c2019
_aCambridge
300 _axiii, 574p.
520 _aThis text is intended to provide undergraduate and first-year graduate students with an introduction to the principles governing the design and performance of rocket propulsion systems. Readers of the text are expected to have a good working knowledge of thermodynamics and the principles of fluid flow in addition to a background in chemistry at least to the college freshman level. Fundamentally, the text has been developed as a compilation of resources from two courses offered at Purdue University: AAE439, Rocket Propulsion and AAE539, Advanced Rocket Propulsion. The former course is taught at the Senior level, while the latter is targeted to Seniors and first year graduate students. The primary emphasis of the text is placed in the area of chemical rocket propulsion systems, the realm that includes solid rocket motors, liquid rocket propulsion devices and hybrid systems that utilize one liquid propellant and one solid propellant. Electric and nuclear propulsion devices are not discussed in detail, but are highlighted briefly within this chapter to place them within the broad context of existing or future rocket propulsion devices. Specifically, this book places emphasis on the propellant systems, combustion processes and thermodynamic and fluid flow processes occurring within the rocket combustion chamber and nozzle. In addition, overall system sizing is presented as well as the interaction of propulsion system performance with vehicle trajectory calculations. Control and structural aspects of a rocket are not considered in detail in this course, but structural issues and sizing considerations are discussed at a mainly conceptual level"--
650 _aJet propulsion
650 _aRocket engines
700 _aHeister, Stephen D.
700 _aAnderson, William E.
700 _aPourpoint, Timothée
700 _aCassady, Joseph R.
942 _cBK
_01
999 _c560716
_d560716