1 publication

• Published Subscription 29 May 2021

  Mathematical modelling of Thrust profile and Kinematic parameters of Launch abort system

  By Md. Saquib Reza, Aanif Hussain, K. Devaki

  Abstract: The paper discusses a mathematical approach for analysis of thrust and related kinematic parameters produced by abort/escape motors of Launch abort system (LAS) during the initial seconds of abort sequence. The profile is generated applying simple numerical technique to the equations of thrust and motion during this non-linear process. Thrust value peaks during this phase, making it crucial for safety of LAS and the crew in particular. Computations involving data …

  Published in Journal of Aerospace Engineering & Technology · Vol. 11, Issue 1, 2021 · pp. 33–47 Read article →