SOUNDING ROCKET FOR ATMOSPHERIC STUDIES
Date
2024-03
Journal Title
Journal ISSN
Volume Title
Publisher
I.O.E
Abstract
Sounding rockets hold a critical role in atmospheric exploration by facilitating the gathering
and examination of various atmospheric factors like temperature, pressure, humidity,
and chemical composition. The primary objective of this project is to conduct
tests on the payload deployment system within a sounding rocket. The key challenges
include developing a motor that is safe, reliable, and consistently performs as
expected, as well as creating a recovery system, such as parachute deployment, capable
of withstanding the demanding conditions of launch and subsequent high-speed or
high-altitude flight. The study centers on the comprehensive design and development
of rockets from scratch, encompassing the propulsion system, motor, and propellant, as
well as the recovery system featuring a deployment mechanism and parachute, all built
entirely from the ground up. Additionally, fully constructed avionics and payload systems
are included. Specifically, a propulsion system capable of hoisting an 8-kilogram
vehicle to an altitude of 1000 meters has been designed and manufactured, with the potential
for further enhancements to increase altitude capabilities. Moreover, a versatile
vehicle capable of conducting missions involving payload deployment and achieving
full recovery with a built-in parachute deployment mechanism has been constructed.
Description
Sounding rockets hold a critical role in atmospheric exploration by facilitating the gathering
and examination of various atmospheric factors like temperature, pressure, humidity,
and chemical composition.
Keywords
Sounding rockets, Payload deployment, Recovery system, Propellant