Portable Rocket Propulsion Analysis Lite Crack+ Patch With Serial Key Free Download
Computer-assisted analysis of multi-stage rocket engines.
Enter the pressure of the combustion chamber, nozzle exit conditions, nozzle shape, propellant mixture, throttle settings, ambient conditions, nozzle inlet or outlet conditions, engine and nozzle (or nozzle sub-module) efficiency, distance/time integration mode, integration interval, integration interval setting, integration step, integration step size, gas constant, gravity and initial temperature.
Calculates all thermodynamic characteristics including pressure profile, thrust, specific impulse and nozzle efficiency.
CAD files can be saved as.cfl and.cfg, ASCII files as.inp.
No need for computer-assisted design (CAD) file generation, or extensive knowledge about rocket engines and thermodynamic analysis.
Adjustable engine parameters including nozzle efficiency, nozzle outlet conditions, propellant mixture composition, ignition/de-ignition conditions and throttle settings.
Optional combustion chamber pressure profiles: perfect for testing theoretical performance in impossible but interesting cases.
Classic laser facility simulation in several nozzle shapes (cone, square) with 4-stage rocket, without any limit of the number of stages.
Independent of the number of stages of the rocket, but in practice, it is limited by computer resources.
"Express" analysis mode allows the user to test the performance of the theoretical rocket by just modifying the engine parameters.
Plenty of sampling rate settings: change the sampling rate for total time, or for the evolution of the thrust, specific impulse or energy.
This simulates the transfer of the rocket thrust to the nozzle, and calculates the energy and propellant consumption.
From ambient conditions to engine operation.
Allows the user to add their preferred ambient conditions to the analysis.
The simulation can be run in both single- or multi-stage rocket modes (with or without staging).
The software can be used for the analysis of stationary rockets, rockets with counter rotation or rockets in free flight.
Performs analysis in several integrated distance/time intervals or in a fixed time scale.
Recover position, velocity, altitude, phase angle and velocity-angle at any time, analyzes and compares the current flight with previous runs.
Allows the user to save time series of data in.xls files.
Can be stopped after the integration has been run for all time, or just before a given time has been reached.
Calculates not only the performance of the engine, but also the mass loss or the energy lost.
Direct fuel consumption analysis.
Analy
Portable Rocket Propulsion Analysis Lite Free For PC
Introduction
Systems and methods of this disclosure provide various methods, systems, and computer program products for defining a reference point system for use in determining location information of at least one user device with respect to a geographical location.
In various embodiments of the above-described subject matter, a user device is configured to define a user device location in a first geographic location. The user device is also configured to define a second geographic location. Furthermore, a reference point system is provided that is configured to determine, based on a defined location of the user device, the location of the user device relative to the defined first geographic location.
In various other embodiments of the above-described subject matter, the reference point system is coupled to a single source of location information.
In various further embodiments of the above-described subject matter, the reference point system is coupled to a network of at least one node capable of receiving location information from at least one of the user device and multiple sources of location information.
In various additional embodiments of the above-described subject matter, the reference point system is configured to store a plurality of references points, wherein each reference point includes location information of at least one of the user device and an associated geographic location.
In yet other embodiments of the above-described subject matter, a multi-modal reference point definition is provided. The reference point system includes a first reference point system and a second reference point system. The first reference point system is configured to detect signals provided by a first user device and to determine a geographical location of the first user device. The first reference point system also provides a first type of reference point. The second reference point system is configured to detect signals provided by a second user device and to determine a geographical location of the second user device. The second reference point system also provides a second type of reference point. The first reference point system, the second reference point system, and one or more additional reference point systems are configured to provide references points that each have a different shape.
In still further embodiments of the above-described subject matter, a user device is configured to enter a first type of signal. The reference point system provides a first reference point having location information based on the first type of signal. The reference point system is also configured to provide a second reference point having location information based on the first type of signal.
In some embodiments, a method of providing location information is provided. The method includes defining a reference point system. The reference point system is configured to detect signals provided by a first user
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