Development of Safety Processes for Design and Manufacture of Small Liquid Propellant Engines and Launch Vehicles
Abstrak
The Cal Poly Pomona (CPP) Liquid Rocket Lab project teams in the 2020-2021 academic year further developed the planning of the engine injector water flow testing, oxygen compatibility and cleaning procedures and further advanced the Mobile Rocket Engine Test Stand piping and structural design. Failure Modes and Effects Analysis were also performed on the system elements to be able to target the critical components for failure mitigation design and procedure development. The CPP revised system for FMEAs is shown. These items were needed to be accomplished in order to perform an engine hot firing for the Bronco 1 Launch Vehicle. This paper describes briefing some the status of the CPP FAR-Mars competition progress and the vehicle systems manufacturing and assembly modifications related to safety developed during our program activity. Some of our testing objectives were postponed due to the COVID19 activity constraints. © 2021, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.
Topik & Kata Kunci
Penulis (1)
F. Chandler
Akses Cepat
- Tahun Terbit
- 2021
- Bahasa
- en
- Total Sitasi
- 1×
- Sumber Database
- Semantic Scholar
- DOI
- 10.2514/6.2021-3273
- Akses
- Open Access ✓