FIELD: physics.
SUBSTANCE: method is implemented by using a simulator in form of a captive-carry training missile which is in form of massive model of a real rocket comprising two blocks: a central module and an electronic load unit. The central module consists of a microprocessor-based device with a digital data and one-time command input/output module, internal memory for recording information on flash memory and an electronic load unit. The electronic load unit simulates current consumption of a real rocket. The internal memory enables to conduct post-flight analysis of activities of the flight personnel. The central module and the electronic load unit lie in the massive model while observing weight and centring characteristics and optimum conditions for heat removal. The device is powered by an onboard 27 V power supply. Said method is realised using the said device.
EFFECT: high reliability of modelling use of a rocket in real flight conditions.
3 cl, 2 dwg
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Authors
Dates
2011-06-27—Published
2009-09-07—Filed