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No 3 (2023) Technical mechanics
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UDC 621.002.56
Technical mechanics, 2023, 3, 58 - 67
FEATURES OF EXPECTED COST ESTIMATION FOR R&D’S ON SPACECRAFT DEVELOPMENT
DOI:
https://doi.org/10.15407/itm2023.03.058
Sazina N. P., Zhukova L. H.
Sazina N. P.
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
Zhukova L. H.
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
The aim of this work is to identify the features of expected cost estimation for R&D’s on spacecraft
development.
The study is based on a methodological approach to expected cost estimation for R&D’s on spacecraft
development. The cost estimation model is based on a method of componentwise analogy for relatively
simple spacecraft components, moving along the edges of a weighted oriented tree graph that models
the spacecraft technical structure, and fuzzy mathematics methods. The methodological approach will
allow one to obtain required R&D expected cost indices early in the spacecraft development when the
standardized cost estimation method and parametric methods are difficult to use because of the
insufficiency of bug-free design and manufacture documentation and statistical data on labor
intensiveness and materials consumption.
The design novelty, R&D complexity, and work automation coefficients are determined by converting the
index value from a fuzzy number in a fuzzy interval into a crisp number, thus allowing one to reduce
the effect of subjective factors.
Calculating the engineering-and-economical indices of a spacecraft by all R&D participants using the
same methodological approach increases the accuracy and shortens the time of the computational process.
Conducting the calculations in a systematic way will fill the statistical base of the space sector with
labor intensiveness and materials consumption data needed for estimating the cost of new spacecraft and
components thereof using a unified concept package – a glossary.
The paper presents the operation sequence of estimating the cost of R&D on spacecraft development and
describes the required input data and the output data format.
cost estimation model, R&D, procedure, spacecraft, cost estimation
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https://doi.org/10.15407/knit2012.05.066
2. Marchenko V. T., Petliak O. A., Sazina N. P., Khorolskyi P. P. Methodological approach to spacecraft development cost calculation. Teh. Meh. 2021. No.3. Pp. 83-98. (in Ukrainian).
https://doi.org/10.15407/itm2021.03.083
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4. Marchenko V. T., Petliak E. P., Sazina N. P., Khorolskyi P. P. Quantitative assessment of the technical level of space systems of Earth remote sensing and geostationary satellite communication systems. Teh. Meh. 2019. No. 4. Pp. 92-106. (in Russian).
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5. Marchenko V. T., Khorolskyi P. P., Sazina N. P., Zhukova L. H. Algorithm to assess the technical level ofremote Earth sensing spacecraft. Teh. Meh. 2017. No. 4. Pp. 41-48. (in Russian).
https://doi.org/10.15407/itm2017.04.041
Copyright (©) 2023 Sazina N. P., Zhukova L. H.
Copyright © 2014-2023 Technical mechanics
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