1. Huber, Paul W. Hypersonic Shock-Heated Flow Parameters for Velocities to 46,000 feet per second and Altitudes to 323,000 feet. NASA Technical Report NASA-TR-R-163, LangleyResearchCenter,December1963.
2. Physics of Explosion, Under the editorship of Orlenko,L.P. issue 3, augmented edition - V.1-M.,FIZMATLIT,2004.832pp.ISBN59221-N50219-2(RussianSource)