A mathematical model of heat shielding for a nose cone taking into account critical flight situations

Author:

Urazbakhtin F. A.,Kharinova Yu. Yu.,Urazbakhtin V. F.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference5 articles.

1. Urazbakhtin, F.A., Control of Critical State Way Out at Technical Device Operation, Avtomatizatsiya i Sovremennye Tekhnologii, 1998, no. 11, pp. 15–20.

2. Avdonin, A.S., Raschet na prochnost’ kosmicheskikh apparatov (Strength Analysis of Spacecraft), Moscow: Mashinostroenie, 1979.

3. Balabukh, L.I., Kolesnikov, K.S., Zarubin, V.S., et al., Osnovy stroitel’noi mekhaniki raket (Fundamentals of the Structural Mechanics of Rockets), Moscow: Vysshya Shkola, 1969.

4. Urazbakhtin, F.A., Multicretiriality at Operation of Complex Technical Devices, Avtomatizatsiya i Sovremennye Tekhnologii, 1996, no. 12, pp. 5–8.

5. Urazbakhtin, A.Yu., Modelling of Critical Situations at Cutting Workpieces for Shaping Parts of Solid Propellant Engine Igniters, Intellektual’nye Sistemy v Proizvodstve, 2012, vol. 20, no. 2, pp. 69–76.

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