RocketPy: Six Degree-of-Freedom Rocket Trajectory Simulator

Author:

Ceotto Giovani H.1ORCID,Schmitt Rodrigo N.2,Alves Guilherme F.3,Pezente Lucas A.4,Carmo Bruno S.5ORCID

Affiliation:

1. Masters Student, Dept. of Mechanical Engineering, Escola Politécnica of the Univ. of São Paulo, Av. Prof. Mello Moraes, 2231, São Paulo 05508-030, Brazil (corresponding author). ORCID: .

2. Masters Student, National Institute for Space Research, Av dos Astronautas 1758, Sao Jose dos Campos, Sao Paulo 12227-010, Brazil.

3. Undergraduate Student, Escola Politécnica of the Univ. of São Paulo, Av. Prof. Mello Moraes, 2231, São Paulo 05508-030, Brazil.

4. Undergraduate Student, Institute of Mathematics and Statistics of the Univ. of São Paulo—R. do Matão, 1010, São Paulo 05508-090, Brazil.

5. Associate Professor, Dept. of Mechanical Engineering, Escola Politécnica of the Univ. of São Paulo, Av. Prof. Mello Moraes, 2231, São Paulo 05508-030, Brazil. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference23 articles.

1. Aitoumeziane, A., et al. 2019. Traveler IV apogee analysis. Los Angeles: USC Rocket Propulsion Laboratory.

2. Alves G. F. G. H. Ceotto R. N. Schmitt and L. A. Pezente. 2020. “Projeto-Jupiter/RocketPaper.” Accessed November 21 2020. (11).

3. Apogee Rockets. 2020. “RockSim information.” Accessed December 5 2020. https://www.apogeerockets.com/RockSim/.

4. Astos Solutions GmbH. 2018. “ASTOS—Analysis simulation and trajectory optimization software for space applications.” Accessed November 25 2020. https://www.astos.de/products/astos.

5. Barrowman J. S. 1967. “The practical calculation of the aerodynamic characteristics of slender finned vehicles.” Ph.D. thesis Dept. of Aerospace Engineering Catholic Univ. of America.

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