1. Harrje, D.T.: Historical survey. In: Harrje, D.T., Reardon, F.H. (eds.) Liquid Propellant Rocket Combustion Instability, pp. 30–34. NASA, Washington, DC (1972)
2. Dutheil, J.-P., Bou, Y.: Highly reusable LOx/LCH4 ACE rocket engine designed for spaceplane: technical maturation progress via key system demonstrators results. In: 7th European Conference for Aeronautical and Space Sciences (2017)
3. Watanabe, D., Tamura, T., Onga, T., Manako, H., Negoro, N., Kurosu, A., Kobayashi, T., Okita, K.: Hot-fire testing of LE-X thrust chamber assembly. In: ISTS, Kobe, Japan. Mitsubishi, JSASS (2015)
4. Hulka, J., Hutt, J.J.: Instability phenomena in liquid oxygen/hydrogen propellant rocket engines, volume 169 of progress in astronautics and aeronautics. In: Yang, V., William, A. (eds.) Liquid Rocket Engine Combustion Instability, pp. 39–72. AIAA, Washington, DC (1995)
5. Jensen, R.J., Dodson, H.C., Claflin, S.E.: Lox/hydrocarbon combustion instability investigation. Technical Report NASA-CR-182249, Rocketdyne Division, Rockwell International (1989)