event
MS Proposal by Rithvik Nagarajan
Primary tabs
Rithvik Nagarajan
(Advisor: Prof. Lightsey)
will propose a master’s thesis entitled,
Numerical Studies on the Determination and Prevention of Roll Resonance in Liquid Sounding Rockets
On
Thursday, February 1 at 11:00 a.m.
Weber Space and Technology Building 304
Abstract
Sounding rockets are suborbital vehicles designed to carry scientific payloads and perform
experiments in the upper atmosphere. Recently, there has been a focus on reusable liquid sounding
rockets to allow faster launch rates and lower costs per mission. Fin-stabilized sounding rockets
tend to be designed with high length-to-diameter ratios for drag optimization. This leads to a
susceptibility in roll-yaw resonance, where the vehicle spins close to the pitch natural frequency.
Previous studies have shown the vehicle can exhibit abnormal rolling and yawing motion beyond
predictions by linear theory. These phenomena are referred to as roll lock-in and catastrophic yaw
respectively. These effects can destabilize the rocket and induce high structural loads.
This research investigates the susceptibility and consequences of roll lock-in and catastrophic yaw
on liquid sounding rocket designs using a comprehensive a 6DOF numerical model. Non-linear
combustion, vehicle aeroelasticity, configurational asymmetries, and non-linear aerodynamics are
incorporated into this model with Monte Carlo variables. Previous off-nominal Georgia Tech sounding
rockets are studied with respect to roll resonance to validate this model. This numerical approach
is used to validate a well- known space-shot sounding rocket design and assess mission failure
likelihood. The findings reveal a high susceptibility to roll resonance, prompting the proposal of
a roll control scheme that takes advantage of liquid rocket pressurized gas. Four attitude control
thrusters are fired in pairs, implementing a bang-bang roll control scheme tailored for liquid
sounding rockets with elevated roll resonance risk. This research analyzes the effectiveness of the
control system in mitigating roll resonance issues.
Committee
• Prof. Glenn Lightsey – School of Aerospace Engineering (advisor)
• Prof. Jonathan Rogers – School of Aerospace Engineering
• f Aerospace Engineering
Groups
Status
- Workflow Status:Published
- Created By:Tatianna Richardson
- Created:01/25/2024
- Modified By:Tatianna Richardson
- Modified:01/25/2024
Categories
Keywords
Target Audience