![]() | Two propellant grains for the "B-200" motor, used for static (ground) tests of the rocket motor. One of the goals of the AST series of static tests was to determine the optimum oxidizer/fuel ratio for the propellant. The upper grain in the photo had a oxidizer/fuel ratio of 60/40, and the lower grain, a ratio of 75/25. Note the colour difference--the greater the oxidizer percentage, the darker the colour. |