11. Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation

11. Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation

Ushkin N. P., Moroz V. G., Tikhaya M. V.

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Kosm. teh. Raket. vooruž. 2016 (1); 68-75
 
Language: Russian
Annotation:
The factors are considered that have an impact on the value and behavior of SRM flow rate and thrust characteristics after stage separation (in the leg of deep decay). It is shown that thrust behavior in the leg of deep decay is determined by two main processes: afterburning of solid propellant charge residues within the first 3-5 s and mass input of internal thermal protection coating destruction products within the following several tenths of second. The dependences are proposed for design evaluation of SRM intra-ballistic and flow rate/thrust characteristics.

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