19. Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation
Organization:
Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
Page: Kosm. teh. Raket. vooruž. 2017 (2); 107-111
Language: Russian
Annotation: The paper presents the generalized experience of designing and development testing of the pneumatic system for nose aerodynamic fairing halves jettisoning. The algorithm of its parameters calculation is given. The satisfactory convergence of the pneumatic system parameters calculation results with the experimental data from the ground and flight tests is shown.
Key words:
Bibliography:
1. Basis of Calculation of Gas Parameters in Pneumatic Systems Operation: Teacher Edition of Yuzhnoye SDO. 21.7217.123 ОТ. 1988.
2. Cyclone-4 SLS. Analysis of Experimental Data on PLF Doors Jettison Pneumatic System: Technical Report / Yuzhnoye SDO. Cyclone-4 21.17689.213 ОТ. 2014.
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