RPA – Tool for Rocket Propulsion Analysis
Home Licensing Downloads Contact

Screenshots

RPA Standard Edition

Click any image to enlarge it


Engine definition

Nozzle flow model: nozzle condition

Chamber geometry: design parameters

Chamber geometry: size and geometry

Chamber geometry: created DXF file opened in QCad

Propellant analysis

Propellant analysis plot

RPA Standard and Lite Editions

Click any image to enlarge it


Engine definition

Dialog window "About RPA"

Propellant specification

Dialog window "Components"

Nozzle flow model: nozzle condition

Nozzle flow model: nozzle shape and efficiencies

Nozzle flow model: Ambient Conditions / Throttle settings

Chamber performance: thermodynamic properties

Chamber performance

Chamber performance: altitude performance

Chamber performance: throttled performance

Plot - throttled engine performance

Plot - altitude performance

Plot - altitude performance with flow separation

Nested analysis

Nested analysis: plot

Species database viewer/editor

Dialog window "Preferences"

Dialog window "RPA log"

Copyright © 2009-2011 Alexander Ponomarenko  |  Contact  | 
Last modified: February 22, 2011