Abstract—The paper presents some aspects regarding the mathematical model and performance evaluation for a two stages strap-on boosters launcher. This work uses two separate models dedicated for each flight phase. For the ascending phase, we will use a three degrees of freedom model in quasi–velocity frame. For the orbital phase, we will use a Gauss perturbing model. The results analysed will be in quasi-velocity frame but also some orbital parameters will be presented. Using these models, the strap-on boosters launcher performances will be evaluated. The novelty of the paper consists in orbital injection approach, with optimal manoeuvre description
Index Terms—Mathematical model, orbital injection, strap-on booster launcher performances.
Teodor-Viorel Chelaru is with University Politehnica of Bucharest, Romania (e-mail: teodor.chelaru@upb.ro).
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Cite: Teodor-Viorel Chelaru and Adrian Chelaru, "Mathematical Model for Strap-on Boosters Launcher, Performances Evaluation," International Journal of Modeling and Optimization vol. 7, no. 3, pp. 122-127, 2017.
