AnaSyn®
System of multifunctional computer simulation of LRE
(RF certificate # 960283,
application # 960177 dated 28.06.1996)
Assignment
AnaSyn application
package is intended for the analysis and synthesis of
various cycle of liquid-propellant rocket engines (LRE)
at the stage of concept development and selection of main
parameters.
The software product is convinient
tools for the engeneers and designers, working over LRE
creation. To work the AnaSyn complex
professional training in the field of rocket engines and
also small experience of operator-personal computer
dialogue are necessary.
AnaSyn computerizes the process
of engineer's work over LRE cycle, helping him to decide
two problems of its designing: the problem of cycle
creation (problem of synthesis) and the problem of its
thorough analysis.
Analysis +
Synthesis =
AnaSyn
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Application package allows the designer:
to generate the library of various
LRE;
To enter a new cycle into the
library;
to update of any cycles available
in the library;
to create a mathematical model of
new engine cycle;
to request the necessary initial
information;
to carry out the balance
calculation of engine with specified accuracy;
to carry out a design and select
overall dimensions of main units of the engine,
namely:
- pumps
- throttles
- gas generator
- gas turbines
- combustion chamber
- liquid-propellant turbines
- cooling passages
- injectors head
to make autonomous analysis of
thermo-physical properties of any substance,
contained in the AnaSyn data
bank;
to make autonomous thermodynamic
analysis of combustion products of bipropellant
and tripropellant avaiable in the AnaSyn
data bank;
to make the calculation of engine
control ranges on pressure and mixture ratio in
the combustion chamber;
to create diagrams of parameters
correlation for different operational modes.
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