TY - JOUR
T1 - Cost Model for CubeSat Projects in Mexico
AU - Jiménez Navarro, E. N.
AU - Solís Santomé, A.
AU - Padilla Pérez, D. A.
AU - Domínguez Pacheco, F. A.
AU - Sosa Paz, C. J.
AU - Silva Sánchez, C.
N1 - Publisher Copyright:
© Published under licence by IOP Publishing Ltd.
PY - 2023
Y1 - 2023
N2 - This work focused on designing a cost estimation model in the area of space engineering for the development of nanosatellite projects in Mexico. See employed the use of methodologies such as Hall and Jenkins, software engineering cost estimating methodology, as well as project management methodology. Similarly, the COSYSMO methodology and parametric cost methodology were incorporated to guide this research towards the space sector. The estimation results are based on satellite engineering equations and forecasts of the inflation factor. Finally, a graphical user interface named SACANI was obtained. Allowing the estimating a nanosatellite project by "integration of components"or by "research and development". The first asks the user for the components by subsystem through drop-down lists, giving a breakdown of the estimated costs for the CubeSat, development phases and ground station, according to the data provided by the interested party. The second model is more robust because it requests the type of project, the category, the amount of CubeSat required, the year to estimate the cost, the mass of the payload, among other data. Similarly, both models yield a previous result of the estimate made according to the data entered by the project estimator.
AB - This work focused on designing a cost estimation model in the area of space engineering for the development of nanosatellite projects in Mexico. See employed the use of methodologies such as Hall and Jenkins, software engineering cost estimating methodology, as well as project management methodology. Similarly, the COSYSMO methodology and parametric cost methodology were incorporated to guide this research towards the space sector. The estimation results are based on satellite engineering equations and forecasts of the inflation factor. Finally, a graphical user interface named SACANI was obtained. Allowing the estimating a nanosatellite project by "integration of components"or by "research and development". The first asks the user for the components by subsystem through drop-down lists, giving a breakdown of the estimated costs for the CubeSat, development phases and ground station, according to the data provided by the interested party. The second model is more robust because it requests the type of project, the category, the amount of CubeSat required, the year to estimate the cost, the mass of the payload, among other data. Similarly, both models yield a previous result of the estimate made according to the data entered by the project estimator.
KW - Cost
KW - CubeSat
KW - Lifecycle
KW - Methodology
KW - Model
UR - http://www.scopus.com/inward/record.url?scp=85159578137&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/2475/1/012008
DO - 10.1088/1742-6596/2475/1/012008
M3 - Artículo de la conferencia
AN - SCOPUS:85159578137
SN - 1742-6588
VL - 2475
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
IS - 1
M1 - 012008
T2 - 2022 International Conference on AeroSpace Science and Technology, ICASST 2022
Y2 - 28 November 2022 through 2 December 2022
ER -