Solid
Rocket Motor Performance Analysis and Prediction
by
Thiokol, Hercules, Rocketdyne, Purdue University, and NASA scientists and
engineers
This
ultimate textbook tells exactly how to evaluate rocket motor static tests
to determine the best grain geometries, motor configurations, and propellants
for a design of any size. It's the best, most complete and comprehensive
volume of its kind anywhere!
With
these instructions you can make detailed analyses that will predict full-scale
motor performance, by using theoretical performance criteria (from chemical-thermodynamic
information), and the demonstrated performance data obtained from subscale
motor tests, or from previous firings on full-scale motors of similar design.
If you
design, build, test, or use solid propellant rockets, you need this reference
handbook. It's the official NASA design and engineering guide, loaded
with once highly-secret data, parameters, scientific analyses, rocketry
information, and esoteric lore, providing data on all types of rocket and
missile propellant grains.
Fundamental
phenomena and theories are reviewed, and the interrelationships of the
critical performance parameters are explained. It presents methods
for predicting the time histories of motor pressure, thrust, and mass flow,
together with techniques for evaluating the input parameters necessary
for identifying and evaluating performance loss mechanisms of various propellant
systems and with various motor operating conditions.
You'll
learn how to analyze losses upstream and downstream of the nozzle throat,
for their effect on nozzle performance and deliverable specific impulse.
You'll also discover the professional ways to assess test motor characteristics,
determine the number of tests and test conditions needed for a given design.
There's
more! Now you can understand exactly how to scale these parameters
to predict full-scale motor performance! Predicted and demonstrated
propellant and motor performance are correlated and explained in great
detail, showing the necessary techniques and procedures.
Prepared
at the NASA Lewis Research Center by scientists and engineers from Rocketdyne
Solid Rocket Division (North American Rockwell Corporation), Hercules Powder
Company, Purdue University, and Thiokol Chemical Corporation, this valuable
book gives the practical information you need to design and evaluate a
high-technology, state-of-the-art composite solid propellant rocket motor.
The contents
are the result of more than 25 years of investigations by the world's largest
propulsion contractors. Literally billions of dollars were
spent obtaining this critical yet hard-to-find data.
Typical engineering illustrations
(much smaller than in book)

The prediction
of pressure and thrust versus time is analyzed, with attention to internal
flow-field monitoring, prediction of motor mass and motor balance versus
time, evaluation of propellant performance parameters, and prediction of
performance variability.
In a
word, this is the most complete and comprehensive
book ever written about the theoretical
and practical engineering design predictions for solid performance.
It’s thick, heavy, and packed with accurate information for the professional
(and “amateur”) rocket scientist, engineer, technician, and experimenter.
There
are also more than 25 engineering figures, and several tables. Plus
there's a 7-page glossary of nomenclature, symbols, and definitions; 11
pages of technical references (149 different studies are listed);
... and
MUCH
more not mentioned here!
All essential
algebraic formulae and equations are included, working with a wide variety
of common and complex propellants and motor configurations.
If you
design, build, test, or fly rockets or missiles of any size, you'll want
this superb reference textbook. It’s especially useful for “amateur”
rocket builders -- with an abundance of data, esoteric information, and
once-secret lore from the world's foremost rocket builders: Aerojet, Thiokol,
Rocketdyne, Hercules, and NASA.
Very
hard to find and now out-of-print, this new limited edition has been republished
by the Rocket Science Institute. It's printed with a high-resolution
laser printer (not
photocopied) on high-quality, bright-white, acid-free paper for years of
reference use. 106 pages, large and easy-to-read 11" x 8-1/2"
size. ISBN 1-878628-22-4
$24.95
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