Determination of Burnout Velocity and Altitude of N-Stage Rocket Varying with Thrust Attitude Angle

Author:

Bhatnagar Paras,Sharma Rupa Rani

Publisher

Springer Nature Switzerland

Reference25 articles.

1. Peressini, A.L.: Lagrange multipliers and the design of multi-stage rockets. The UMAP J. 7.3 (1986)

2. Bhatnagar, P., Rajan, S., Saxena, D.: Study on optimization problem of propellant mass distribution under restrictive conditions in multistage rocket. In: IJCA Proceedings on International Conference on Advances in Computer Applications 2012, by IJCA Journal ICACA - Number 1 (2012)

3. Chern, J.S., Wu, B., Chen, Y.S., Wu, A.M.: Suborbital and low thermos-spheric experiments using sounding rockets in Taiwan. Acta Astronaut. 70, 159–164 (2012)

4. Coleman, J.J.: Optimum stage weight distribution of multistage rockets. ARS J. 31 (1961)

5. Dief, T.N., Yoshida, S.: System identification and adaptive control of mass-varying quad-rotor. Evergreen Joint J. Novel Carbon Resource Sci. Green Asia Strat. 4(1), 58–66 (2017)

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