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University of Illinois at Urbana-Champaign

Infrared radiation profiles of a hypersonic glide vehicle during re-entry

Abstract

dc:description

An HGV trajectory was calculated for a waverider configuration boosted to an altitude of 60 (km) with a ∆V of 3.7 ( km/s ). For the hypersonic vehicle the total downrange distance was 3250 (km) over a flight time of 21.75 minutes. Using a semi-empirical model for the stagnation point heat flux it was found that the maximum along the trajectory was ̇Q = 4x106 ( W/m2 ). CFD simulations of the HIFiRE-5 flight test vehicle were completed at chosen points along the trajectory and it was found that the semi-empirical model under-predicted the simulated stagnation point values at every location. It is hypothesized that the ratio of wall to total enthalpy plays a significant role in this under prediction and it is shown that as this ratio approaches 0 the results have much better agreement with the semi-emperical model. An in-house CFD post-processing software package (HVBETS) is validated and used to measure the IR signature profile of the vehicle and the high temperature wake. The vehicle surface signature varies between 0.5 and 6.4 ( kW/Sr ) and the wakesignature varies between 8.27x10−5 and 9.97x10−5 ( W/Sr/cm2 ). It is hypothesized that the orders of magnitude difference between the two IR sources is due to the conditions imposed on the wake at an altitude of 70 (km). The ground work for future analysis is laid where the parameters of the wake are changed to increase the total contribution and determine which variables are most important for the IR wake signature.

Degree

thesis:*
Name thesis:degree_name
M.S.
Level thesis:degree_level
Thesis
Discipline thesis:degree_discipline
Aerospace Engineering
Grantor
University of Illinois at Urbana-Champaign
Year dc:date
2023

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Thomas, Nathan Robert
Contributors dc:contributor
  • Levin, Deborah A

Subjects

dc:subject × 4

Rights

dc:rights
Statement dc:rights
  • Copyright 2023 Nathan Thomas
Language dc:language
en, eng

Identifiers

dc:identifier.*
Handle dc:identifier
https://hdl.handle.net/2142/120412

Chain of custody

source
Harvested from
University of Illinois - Urbana-Champaign
Base URL
www.ideals.illinois.edu/oai-pmh
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Thomas, Nathan Robert. Infrared radiation profiles of a hypersonic glide vehicle during re-entry. Thesis thesis, University of Illinois at Urbana-Champaign, 2023. https://hdl.handle.net/2142/120412