CS-062: Lightweight Pressure Regulator for Space Launch Vehicles
This case study focuses on the design of a regulator for a suborbital launch vehicle developed by the Aerospace Systems Research Institute, utilizing Flownex to simulate and ensure a consistent flow rate of pressurized helium to maintain constant LOX tank pressure during blowdown.
Share This:
Share This:
More Case Studies
You might also be interested in these CASE STUDIES
CS-070: Quantifying the Effect of Condenser Tube Foaling on Power Plant Thermal Efficiency
This case study focuses on using Flownex to assess how condenser tube foaling affects thermal efficiency and increases operational costs in a coal-fired power plant.
CS-069: Investigating a Delay in O2 Response in an Air/Fuel Gas System
This case study investigates a delay in airflow response during transient load changes in a fossil fuel power station, where Flownex SE identified that optimizing feedforward control and
CS-068: Energy and Exergy in a Brayton Cycle-Based Power Conversion Unit
This case study simulated a Brayton cycle PCU in Flownex SE under steady-state conditions, logging parameters to calculate energy and exergy, and testing fault conditions by adjusting component
CS-067: Design of Low Temperature Proton Exchange Membrane Fuel Cell System Components
This case study demonstrates the use of Flownex to model system components of a low-temperature proton-exchange membrane fuel cell (PEMFC), including the cathode-side air flow…
CS-066: Data Centre Free Cooling Analysis Using Flownex SE
This case study demonstrates how Flownex SE simulates free cooling in a data center using natural resources and weather data in a transient analysis to optimize…
CS-065: Validating a Scaling Procedure for Cryogenic Pressure Fluctuations
This case study illustrates how Flownex was used with a scaling procedure based on dimensional analysis to simulate transient pressure fluctuations in a scaled cryogenic fluid flow system,