Hydroxyl-terminated polybutadiene (HTPB) is a common ingredient in rocket propellants, but
its thermochemical properties (composition, density, and heat of formation) are not well …

To develop sounding rockets that can be used for various missions, a university, research
center, and two enterprises collaborated to conduct a critical-system development project on …

View Video Presentation: https://doi. org/10.2514/6.2021-1971. vid Hydroxyl-terminated
polybutadiene (HTPB) is a common ingredient in rocket propellants, but its thermochemical …

A feasibility study of the design of multiport solid fuel using the ratio of the nozzle throat area
to the port area was performed in a hydrogen peroxide/high-density polyethylene hybrid …

I. Introduction ybrid rocket motors are well known in space community for their intrinsic safety
due to the storage of oxidizer and fuel in separated tanks, overall system simplicity …

I. Introduction he fundamental principle of hybrid rocket is that a gas or liquid oxidizer is
injected into the solid fuel port and flame is generated; and the solid fuel is vaporized by …

Experimental testing was conducted to investigate the behavior of polyoxymethylene (POM)
for consideration as the solid fuel component in an upper stage hybrid rocket engine using …

The study and use of green propellants for aerospace applications is becoming more
prevalent. HAN based mono-propellant, AF-M315E, has been considered for different …