Description: From Summary: "A flight investigation was made of a supersonic twin-ram-jet test vehicle using short-flame-length burners. The test demonstrated a maximum acceleration of 3.6g and a maximum flight Mach number of 3.02. Data were obtained over a Mach number range from about 1.9 to 3.0, an altitude range from 1,800 to 40,900 feet, and a fuel-air-ratio range from 0.012 to 0.065."
Date: September 15, 1950
Creator: Faget, Maxime A. & Dettwyler, H. Rudolph
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department