19. Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation

19. Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation

Kabakova Zh. V., Kuda S. А., Logvinenko А. I., Khomyak V. А.

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

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.

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.

Full Text(PDF) Content 2017 (2)