What's new in Rocket Propulsion Analysis Lite 1.2.8
Apr 28, 2015
- Mistake is fixed in estimation of chamber performance with flow separation in the nozzle
New in Rocket Propulsion Analysis Lite 1.2.7 (Apr 28, 2015)
- Mistake is fixed in Thermodynamic Database Editor that was preventing the saving of user-defined species
- Improved support of editing and handling of user-defined species in Thermodynamic Database Editor
- C++ library Eigen is used as a standard solver of system of linear equations
- RPA for Windows is built with MS VC++ 2010 and Qt 4.8.3
New in Rocket Propulsion Analysis Lite 1.2.5.2 (Apr 28, 2015)
- Fixed mistake in definition of nozzle exit condition in throttled performance analysis
- Fixed mistake in calculation of thrust in throttled performance analysis
- Improved thrust level discretization in throttled performance analysis
- Improved pressure discretization in altitude performance analysis
New in Rocket Propulsion Analysis Lite 1.2.5 (Apr 28, 2015)
- Note that RPA Lite Editions v.1.2.2 - 1.2.4 have never been released
- Fixed mistake in calculation of nozzle exit condition for reaction products with "liqud-solid" phase transition
- Improved filter functionality in species dialog window (ported from RPA SE 1.2.4)
New in Rocket Propulsion Analysis Lite 1.2.1 (Apr 28, 2015)
- Improved performance estimation for solid propellants
- Fixed mistake in calculation of sonic velocity at nozzle throat section for reaction products with condensed phase