1. A Century of Ramjet Propulsion Technology Evolution
2. HillP.PetersonC., Mechanics and Thermodynamics of Propulsion, 2nd ed., Addison Wesley Longman, Reading, MA, 1992, pp. 141–216.
3. Parachute system to recover spinning (250 rps) 155-mm shell subjected to 20,000 g's launch conditions
4. SOLID FUEL RAMJET COMBUSTOR DESIGN
5. NuscaM. J.OskayV. “Comparison of Computational Analysis with Flight Tests of a 40 mm Solid-Fuel Ramjet Projectile,” U.S. Army Ballistic Research Lab. Rept. ADA206536, Aberdeen, MD, 1989, p. 45.