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Clayton Huggett | C. E. Bartley | Mark M. Mills

Solid Propellant Rockets

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A01=C. E. Bartley
A01=Clayton Huggett
A01=Mark M. Mills
Adiabatic flame temperature
Age Group_Uncategorized
Age Group_Uncategorized
Ampere
Artillery
Author_C. E. Bartley
Author_Clayton Huggett
Author_Mark M. Mills
Autoignition temperature
automatic-update
Ballistite
Black-body radiation
Burn rate (chemistry)
Burnup
Carbon monoxide
Catalysis
Category1=Non-Fiction
Category=PH
Category=PHFC
Category=THF
Category=TRP
Category=TTDS
Chain reaction
Chamber pressure
Characteristic velocity
Combustion
Combustion chamber
Convection
COP=United States
Cordite
Cryogenics
Delivery_Delivery within 10-20 working days
Detonation
Discharge coefficient
Effective temperature
Entropy of activation
eq_isMigrated=2
eq_non-fiction
eq_science
Exothermic process
Flame speed
Formaldehyde
Fuel
Gas composition
Gas constant
Gasification
High pressure
Hot particle
Ideal gas
Ideal gas law
Induction period
Internal ballistics
Isochoric process
Language_English
Liquid fuel
Liquid-propellant rocket
Mach number
Nitrocellulose
Nitroglycerin
Nitrous oxide
Nozzle
Oxidizing agent
PA=Available
Poisson's ratio
Potassium perchlorate
Price_€20 to €50
Propellant
Propulsive efficiency
PS=Active
Rate-determining step
RDX
Reagent
Refractory
Resonance
Reynolds number
Rocket
Rocket engine
Rocket propellant
Safety factor (plasma physics)
Smokeless powder
softlaunch
Specific impulse
Stefan–Boltzmann constant
Stokes' law
Surface layer
Tetryl
Thermal decomposition
Thermal expansion
Thermodynamic equilibrium
Thermosetting polymer
Volumetric efficiency
Water gas

Product details

  • ISBN 9780691626185
  • Weight: 255g
  • Dimensions: 152 x 235mm
  • Publication Date: 08 Dec 2015
  • Publisher: Princeton University Press
  • Publication City/Country: US
  • Product Form: Paperback
  • Language: English
Delivery/Collection within 10-20 working days

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Description
Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.