Works on: Windows 10 | Windows 8.1 | Windows 8 | Windows 7 | Windows XP | Windows 2000 | Windows 2003 | Windows 2008 | Windows 98 | Windows ME | Windows NT | Windows 95 | Windows Vista | Windows 2012 SHA1 Hash: f973678459d768814c071318070539bea9c5a6cb Size: 1.44 MB File Format: exe
Rating: 2.347826086
out of 5
based on 23 user ratings
Publisher Website: External Link Downloads: 190 License: Demo / Trial Version
Grain Design Program Pro is a demo software by AED and works on Windows 10, Windows 8.1, Windows 8, Windows 7, Windows XP, Windows 2000, Windows 2003, Windows 2008, Windows 98, Windows ME, Windows NT, Windows 95, Windows Vista, Windows 2012.
You can download Grain Design Program Pro which is 1.44 MB in size and belongs to the software category Home and Education. Grain Design Program Pro was released on 2010-11-08 and last updated on our database on 2017-04-22 and is currently at version 3.03.
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Grain Design Program Pro Description
Grain Design Program Lite (GDP) is capable of calculating all 2D-grains, like stars, moonburners, slotted grains, and BATES grains. Geometries are devided into four categories as simple stars are treated analytically, simple cylinders (like BATES), treated analytically, and aAll other shapes are calculated graphically. The user provides a file (.pcx, .gif, or .bmp) of the grain. GDP automatically finds burning areas and calculates burnback. This options allows full burn-back, including slivers. Even cracks can easily be drawn with a drawing program, and modeled. Tabular input allows grain input by entering burning area and burning volume as function of burn depth. Full transient burn-back (include ignitor mass flow, and engine filling and blow-down). Each propellant segment can be of a different propellant type. Burn options for each propellant segment (start burning of a segment x seconds after ignition, or start burning of a segment after another segment has burned a certain distance). Nozzle erosion (tabulated input of erosion vs. time). Checks for possible erosive burning of the rocket motor. No total propellant mass limitations.