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Measurement Techniques
Published in: Measurement Techniques 5/2016

23-08-2016 | MECHANICAL MEASUREMENTS

Transducer for Measuring the Flow Rate of Fuel in the Manned Transport Spacecraft Soyuz

Author: S. V. Balakin

Published in: Measurement Techniques | Issue 5/2016

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Abstract

A fuel flow rate transducer design for a manned transport spacecraft is proposed. It is based on the principle of measuring the phase of the useful signal carrier frequency. This scheme significantly improves the stability of the instrument against mechanical interactions and provides more accurate measurements of the amount of fuel consumed by the spacecraft.
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Literature
1.
L. A. Bessonov, Theoretical Foundations of Electricity, Vysshaya Shkola, Moscow (1973).
2.
S. V. Balakin, A. N. Dyvak, and Ya. V. Khachaturov, Patent 2224261 RF, “Means for measuring the impedance of a bridge circuit with close inductive coupling and a device for realizing it,” Izobret. Polezn. Modeli, No. 6 (2005).
3.
S. V. Balakin, A. N. Dyvak, and V. M. Filin, “Phase techniques for level measurements in liquid fuelled rockets,” Datch. Sistemy, No. 1, 5–10 (2005).
Metadata
Title
Transducer for Measuring the Flow Rate of Fuel in the Manned Transport Spacecraft Soyuz
Author
S. V. Balakin
Publication date
23-08-2016
Publisher
Springer US
Published in
Measurement Techniques / Issue 5/2016
Print ISSN: 0543-1972
Electronic ISSN: 1573-8906
DOI
https://doi.org/10.1007/s11018-016-0997-y

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