Stage Separation Analysis of Launch Vehicle Using Monte Carlo Simulation
نویسندگان
چکیده
منابع مشابه
Stage separation dynamic analysis of upper stage of a multistage launch vehicle using retro rockets
K e y w o r d s J e t t i s o n i n g system, Retro-rocket, Jet damping, Pyro, Relative velocity, Relative distance, Launch vehicle. N O M E N C L A T U R E Az launch azimuth (deg) h altitude of separation (km) I inertia tensor (kg-m 2) t Time (s) mM, ms mass of the ongoing and spent bodies (kg) RE, Rp, Rs Earth's equatorial radius, polar radius, radius at the surface (km) r, q, p body angular ...
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ژورنال
عنوان ژورنال: Journal of the Korean Society for Aeronautical & Space Sciences
سال: 2015
ISSN: 1225-1348
DOI: 10.5139/jksas.2015.43.4.341