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Issue: #8 (797)
Aviation, Rocket and Technology
Theoretical and experimental study of thermal conductivity and operational limits of a sodium axial heat pipe relative to the gravity vector orientation
| Authors: Borschev N.O., Kochegarova A.V. | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes |
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| Keywords: axial heat pipe, boiling limit, sonic limit, viscous limit, capillary limit | |
Modelling of CubeSat satellite motion with inflatable braking device. Part 1. Determination of aerodynamic characteristics and trajectory parameters