1. Gazodinamicheskie i teplofizicheskie protsessy v raketnykh dvigatelyakh tverdogo topliva (Gas Dynamic and Thermal Physical Processes in Solid-Propellant Rocket Engines), Koroteev, A.S., Ed., Moscow: Mashinostroenie, 2004.
2. Konstruktsii raketnykh dvigatelei na tverdom toplive (Structures of Solid-Propellant Rocket Engines), Lavrov, L.N., Ed., Moscow: Mashinostroenie, 1993.
3. Hagemann, G., Immich, H., Nguyen, T.V., and Dumnov, G.E., Advanced rocket nozzles, J. Propul. Power, 1998, vol. 14, no. 5, рр. 620–633.
4. Ellis, R.A. and Berdoyes, M., An example of successful international cooperation in rocket motor technology, Acta Astron., 2002, vol. 51, no. 1–9, pp. 47–56.
5. Lacoste, M., Lacombe, A., Joyez, P., Ellis, R.A., Lee, J.C., and Payne, F.M., Carbon–carbon extendible nozzles, Acta Astron., 2002, vol. 50, no. 6, рр. 357–367.