Helium Pressurization Bay

SDSU Rocket Project


As Design Lead for The SDSU Rocket Project, I led the design, assembly, and operation of a new multi-use remote helium pressurization system to safely pressurize the Galactic Aztec Heavy rocket from 200 feet away.

System Operation General Description:

  1. A Helium K-Bottle is connected via a 10' 4000 psi perforated hose to the Helium Pressurization Bay (HPB) inlet.
  2. Before opening the k-bottle, all valves are ensured closed and all regulators unloaded.
  3. Opening the pressure source allows helium to flow into the system, through a 15 micron filter, and into the first regulator with an inlet pressure gauge to show the gauge pressure of the source.
  4. For Galactic Aztec Heavy, the high pressure (~3000 psi) helium is then regulated down to 2000 psi.
  5. This Helium flows to a tee. The main line leads to high flow ball valve and the secondary line leads to a low pressure regulator.
  6. A 200' high pressure line is then connected between the HPB and the rocket. Once the main valve is opened, Helium moves through the line and pressurizes the rocket.
  7. Once the rocket is pressurized and stable, the main valve is closed and a vent valve is opened to vent the main line. A check valve on the rocket would prevent the rocket from depressurizing.
  8. At this point in time, the rocket is fueled and pressurized making it unsafe to approach. The high pressure helium line must be disconnected remotely.
  9. The low pressure regulator allows the user to regulate the helium down to 150 psi. A valve is then opened to allow the low pressure helium to flow through an additional 200' line leading towards the rocket.
  10. This second line is connected to the Helium Release Mechanism (HRM), which uses two actuators to pull down on a high pressure quick disconnect.
  11. The HRM disconnects the main line from the rocket and the rocket is ready to launch.