- Dr. Mark Campbell
- Dr. Mark Psiaki
- Liran Gazit - lg345
The CUSat Satellite project employs Systems Engineering extensively. The Systems group is largely responsible for providing the project with direction by creating top level system requirements, creating best practices, maintaining communications, making design choices, and creating processes for creating a successful product. Each of the subsystem leads also participates as a member of the Systems group, which allows the project to maintain consistency and focus.
|Stephen Cheung - swc34||Melissa Horowitz - mfh24|
|Anders Kelsey - aak26||Jason Rostoker - jer44|
|Brian Rudo - bcr22||Rob Zimmerman - rmz8|
Integration and Testing
The I&T team is responsible for enabling rapid integration and testing of CUSat. I&T is also responsible for testing CUSat in Cornell University's thermal vacuum chamber.
|Bohnish Banerji - bb226||Abhishek Gulati - ag327|
|Kate McGinnis - kam226||Megan Paulette - mep49|
|Garret Touchstone - gdt3||Rob Zimmerman - rmz8|
The Attitude Determination, Control, and Navigation Subsystem (ADCNS) executes the relative navigation that will be used for CUSat's in-orbit inspection procedures. CUSat will primarily be using three GPS boards for attitude determination. For attitude control, CUSat will be using pulsed-plasma thrusters (PPTs) and torque coils. The software portion of ADCNS will consist of the relative navigation algorithms, which will run the various modes of operation defined by the CONOPs.
|Olga Belomstnykh - osb5||David Bunker - dlb97|
|Brandon Chan - bjc54||Patrick Conrad - prc23|
|Shenglong Gao - sg369||Jonathan Guarino - jfg32|
|Rob Kesselman - rjk38||Andrew Knippenberg - ask44|
|Ricky Koontz - rlk35||Scott Linderman - swl28|
|Ian Livingston - isl5||Francisco Moneo-Soler - fm93|
|Wendy Shaun - wxs2||Young Son - yjs9|
|Darren Zanon - djz3|
The camera team is responsible for acquiring images while in orbit, compressing them in a modified JPEG format, and relaying them to the onboard computer, C&DH.
|Maribel Torres-Vidal - mt343||Tommy Tsay - tct4|
Command and Data Handling
C&DH is the central hub for communication and computation on the satellite. Using a commercial off the shelf (COTS) single board computer running Windows CE and C++, C&DH will execute the ADCNS algorithms and flight code.
|Heman Chawda - hkc2||Liwei Chen - lc276|
|Alexander Emmet - ahe7||Daniel Fitzgerald - dpf7|
|Brian Rudo - bcr22|
The GPS team is responsible for the GPS receivers, antennas and algorithms used to calculate sub-centimeter relative positioning.
|Richard Yan - ry35|
The Ground Segment is responsible for the ground operations of the satellite, including ground to satellite communication, tracking and commanding.
|Frank Fort - fcf3||Sam Huang - ch285|
The Harness subsystem is responsible for satellite wiring, the electronics backplane, the electrical interface boards, and any System level electrical concerns.
|Steve Fuertes - saf42||James Maxwell - jem84|
|Robert Nitkin - ran24||Mau Rodriguez - mar97|
The Industry Relations team is responsible for marketing CUSat and seeking commercial and academic sponsorship. If you are interested in sponsoring our project, please see our sponsors page.
|Max Henderson - mwh33|
The propulsion team is responsible for CUSat's pulsed plasma thrusters (PPTs) which give each satellite three degrees of translational freedom and three degrees of rotational freedom.
|Mike Cen - mc373||Aurelien Drevon - ad335|
|Andrew Hall - ajh62||Angie Israni - ai45|
|Xiao Li - xl72||Bei Li Liu - bl222|
|Erfan Parvez - eap43|
The power team is responsible for harnessing solar energy, storing it, and distributing it throughout the satellite.
|Caitlin Carroll - cmc243||Dan Davis - did4|
|Tony Huang - th257||Jarrod Schaeffer - jls284|
The structures team is responsible for designing, analyzing, and manufacturing the body of the satellite as well as the logistics of the internal components.
|Adam Kolozetti - abk43||Richard Larin - rdl27|
|Tim Lin - hl322||Jen Miller - jrm79|
|Jeremy Rosenweig - jpr36||Robert Schatz - res45|
The Survivability team is responsible for analyzing and controlling the satellite's thermal, electrical and vibrational environment on the ground, during launch, and in orbit. Analyzed effects include ESD, atomic oxygen effects, venting and outgassing.
|Tony Li - tyl8||Shawn Xia Liang - xl78|
|Savannah McCoy - sjm63||Ok Joo Park - op29|
Telemetry and Command
T&C is responsible for intersatellite communications as well as satellite to ground communications. T&C uses modified commercial radios operating in amateur frequency bands to transmit images taken by the satellites to the ground station.
|Neha Bansal - nb83||Tyler Dolen - tmd29|