Rocket Propulsion Laboratory
The Rocket Propulsion Laboratory is a student organization at the University of California, San Diego founded in the Spring of 2017.
UC San Diego
Pinned Repositories
ariel-pump
Calculations for Centrifugal Pump Design
Base11-CommandBox
The code for RPL's command box
Base11-FC
Housing our code for Marginal Stability's flight computer running on a Raspberry Pi
Base11-GPS
C++, Verilog, and ASM for the Base 11 GPS.
C.A.M.E.R.O.N.-CAD
Guides
General body of knowledge for Rocket Propulsion Laboratory.
Launchy
Launchy McLaunchface, “Launchy,” is a currently under development by the Rocket Propulsion Laboratory. The launch vehicle is being designed for the FAR | Mars Society Launch Competition in the summer of 2018. Launchy uses the Ariel-1 rocket engine; a LOX/LNG engine achieving 2000 lbf thrust.
marginal-stability
Marginal Stability is a LOx/RP1 powered launch vehicle designed to reach the edge of space at 100 km above the surface!
Remove-Before-Flight
"Remove Before Flight" is a 2000 lbf Liquid Oxygen, Liquid Natural Gas engine currently being designed and developed by the Rocket Propulsion Laboratory. A1’s first static fire is planned for August of 2017.
Unscented-Orientation-Filter
A performance simulation of Crassidis and Markley's unscented quaternion estimator (USQUE) in MATLAB. This is an unscented Kalman filter that keeps track of the orientation of spacecraft. Based on: https://doi.org/10.2514/2.5102
Rocket Propulsion Laboratory's Repositories
rocketproplab/FC_firmware
Launchy Flight Computer Firmware
rocketproplab/Remove-Before-Flight
"Remove Before Flight" is a 2000 lbf Liquid Oxygen, Liquid Natural Gas engine currently being designed and developed by the Rocket Propulsion Laboratory. A1’s first static fire is planned for August of 2017.
rocketproplab/TCA_Computation
For calculating and optimizing the geometry for Thrust Chamber Assemblies
rocketproplab/struct-nose-cone
rocketproplab/SortingHat
rocketproplab/ariel-pump
Calculations for Centrifugal Pump Design
rocketproplab/ignition_static_fire
Ignition Static Fire using Subinitial Stacks
rocketproplab/struct_tps
Thermal Protection System Calculations
rocketproplab/monocoque-bending
Calculating the bending strength of monocoque and semi-monocoque structrues
rocketproplab/jet-spool-calcs
Calculating the number of spools required given compression ratio.
rocketproplab/jetengine
The Rocket Propulsion Laboratory is designing a small turbofan engine that will be used to rapidly characterize the performance of biofuels. The engine will initially be tested and calibrated using Jet A-1 in order to provide a baseline to against which biofuel variations will be compared.