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FSW
Publiclmatlib
PublicGSW
Publicirec-2025-analysis
PublicLiquids-Test-Teensy
Publicliquid-engine-gen
PublicThis script is to be used to develop a small liquid bi-propellant rocket engine. It has been tested to be operational for the design of a 150 [lbf] liquid rocket engine using nitrous oxide and isopropanol as the propellants.report-template
Publicflight-data
PublicGSW-2021
PublicNSW
Publicxpa-avionics
PublicSR-2024-Public-Unsafety
PublicSR2024-xpa7234rit.edu
Publicxpa7234
Publiccalc-factor-of-safety
Public archiveaerospike-generator
Publicirec-2024
PublicLiquids-Test-Stand-Box
Publicbuild-wall-thickness
Public archivecalc-film-coefficient
Public archiveUses pre-calculated interior contour and CEA transport properties to calculate heat transfer coefficient, according to the equation described in source: https://jffhmt.avestia.com/2015/PDF/006.pdfLukewarm-Phoenix
Publicflight-hardware
Publiclaunch-core
Publicradio-module
Publicsensor-module
Public archiveNitron-I
Publicpower-module
PublicRocketPy
Public