Addressing the hypersonic simulation problem

BJ Griffith, JR Maus, BM Majors, JT Best - Journal of Spacecraft and …, 1987 - arc.aiaa.org
THE Wright brothers built a low-speed wind tunnel to simulate the flow over their airplane
and made history in 1903 by making a manned flight last 59 s. Chuck Yeager broke the …

Navier-Stokes simulations of Orbiter aerodynamic characteristics including pitch trim and bodyflap

KJ Weilmuenster, PA Gnoffo, FA Greene - Journal of Spacecraft and …, 1994 - arc.aiaa.org
ON THE entry phase of its first flight, designated Space Transportation System (STS)-l, the
hypersonic pitchingmoment characteristics exhibited by the Shuttle Orbiter were significantly …

Modeling of glow radiation in the rarefied flow about an orbiting spacecraft

SF Gimelshein, DA Levin, RJ Collins - Journal of thermophysics and …, 2000 - arc.aiaa.org
SPACECRAFT radiation is primarily caused by the interaction of spacecraft surfaces with the
rarefi ed atmosphere in low Earth orbit. Detailed information on the physical and chemical …

A method for the experimental characterisation of novel drag-reducing materials for very low Earth orbits using the Satellite for Orbital Aerodynamics Research (SOAR) …

NH Crisp, PCE Roberts, V Hanessian… - CEAS Space …, 2022 - Springer
Abstract The Satellite for Orbital Aerodynamics Research (SOAR) is a 3U CubeSat mission
that aims to investigate the gas–surface interactions (GSIs) of different materials in the very …

[HTML][HTML] Gas concentration in rarefied flows: Experiments and modeling

C Xu, VJ Murray, MD Pilinski… - Aerospace Science and …, 2023 - Elsevier
The relationship between gas-surface scattering dynamics and flow through conical systems
in the rarefied regime has been explored with experimental and computational tools …

Normal and tangential momentum accommodation for Earth satellite conditions

ED Knechtel, WC Pitts - Astronautica Acta, 1973 - ntrs.nasa.gov
Momentum accommodation was determined experimentally for gas-surface interactions
simulating in a practical way those of near-earth satellites. Throughout the ranges of gas …

Assessment of laminar, convective aeroheating prediction uncertainties for Mars-entry vehicles

BR Hollis, DK Prabhu - Journal of Spacecraft and Rockets, 2013 - arc.aiaa.org
TWO important goals for NASA's future Mars exploration programs are to perform a robotic
sample return mission and to enable human exploration missions. Both goals require the …

Modeling of Stardust entry at high altitude, Part 1: Flowfield analysis

ID Boyd, KA Trumble, MJ Wright - Journal of Spacecraft and Rockets, 2010 - arc.aiaa.org
The Stardust sample return capsule entered the Earth's atmosphere at a very energetic
velocity of 12: 6 km= s. In the present study, both continuum (computational fluid dynamics) …

Aerodynamic interactions of a reusable launch vehicle model with different nose configurations

J Jia, D Fu, Z He - Acta Astronautica, 2020 - Elsevier
Abstract The Two-Stage-To-Orbit (TSTO) hypersonic vehicle is an example of a Reusable
Launch Vehicle (RLVs) configuration, and it has the advantages of small mass and large …

[HTML][HTML] Gas-surface interaction effect on round leading edge aerothermodynamics

WFN Santos - Brazilian Journal of Physics, 2007 - SciELO Brasil
Effects of incomplete surface accommodation in rarefied gas flow have been studied by
using the Direct Simulation Monte Carlo (DSMC) method in conjunction with the Cercignani …