SPARCC 3.0 – Solid Propellant CubeSat Propulsion

Authors

Charley Stone, Florida Institute of Technology
Mathieu Cote, Florida Institute of Technology
Evan Carpenter, Florida Institute of Technology
Josh McCarron, Florida Institute of Technology
Tristan Leemon, Florida Institute of Technology
Syd Freiberger, Florida Institute of Technology
Michael Hill, Florida Institute of Technology

Document Type

Poster

Publication Title

Northrop Grumman Engineering & Science Student Design Showcase

Abstract

Objective 1: The team shall build a propulsion system that uses solid propellant. Objective 2: The team shall design a system that will produce variable thrust. Objective 3: The team shall design a propulsion system that meets constraints for a small spacecraft. Constraints: • Mass: 6kg • Power: 16 W • Volume: 2U = 20x10x10 cm

Advisor

Firat Irmak, Eric Swenson, Boris Akhremitchev

Publication Date

4-25-2025

Recommended Citation

Stone, Charley; Cote, Mathieu; Carpenter, Evan; McCarron, Josh; Leemon, Tristan; Freiberger, Syd; and Hill, Michael, "SPARCC 3.0 – Solid Propellant CubeSat Propulsion" (2025). Aerospace, Physics, and Space Science Student Publications. 40.
https://repository.fit.edu/apss_student/40