A review of gas-surface interaction models for orbital aerodynamics applications

S Livadiotti, NH Crisp, PCE Roberts, SD Worrall… - Progress in Aerospace …, 2020 - Elsevier
Abstract Renewed interest in Very Low Earth Orbits (VLEO)-ie altitudes below 450 km-has
led to an increased demand for accurate environment characterisation and aerodynamic …

Research and development of aerospace vehicles with air breathing electric propulsion: Yesterday, today, and tomorrow

AS Filatyev, AA Golikov, AI Erofeev, SA Khartov… - Progress in Aerospace …, 2023 - Elsevier
The main features and key problems in the development of air-breathing electric propulsion
(ABEP) are outlined. Qualitative differences between ABEP and its closest predecessor …

New density estimates derived using accelerometers on board the CHAMP and GRACE satellites

PM Mehta, AC Walker, EK Sutton… - Space Weather, 2017 - Wiley Online Library
Atmospheric mass density estimates derived from accelerometers onboard satellites such as
CHAllenging Minisatellite Payload (CHAMP) and Gravity Recovery and Climate Experiment …

Uncertainty quantification techniques for data-driven space weather modeling: thermospheric density application

RJ Licata, PM Mehta - Scientific Reports, 2022 - nature.com
Abstract Machine learning (ML) has been applied to space weather problems with
increasing frequency in recent years, driven by an influx of in-situ measurements and a …

A review of air-breathing electric propulsion: from mission studies to technology verification

T Andreussi, E Ferrato, V Giannetti - Journal of Electric Propulsion, 2022 - Springer
Air-breathing electric propulsion (ABEP) allows for lowering the altitude of spacecraft
operations below 250 km, in the so-called Very Low Earth Orbits (VLEOs). Operations in …

[HTML][HTML] Satellite drag coefficient modeling for thermosphere science and mission operations

PM Mehta, SN Paul, NH Crisp, PL Sheridan… - Advances in Space …, 2023 - Elsevier
Satellite drag modeling remains the largest source of uncertainty affecting space operations
in low Earth orbit. The uncertainty stems from inaccurate models for mass density and drag …

Modeling satellite drag coefficients with response surfaces

PM Mehta, A Walker, E Lawrence, R Linares… - Advances in Space …, 2014 - Elsevier
Satellite drag coefficients are a major source of uncertainty in predicting the drag force on
satellites in low Earth orbit. Among other things, accurately predicting the orbit requires …

ADBSat: Methodology of a novel panel method tool for aerodynamic analysis of satellites

LA Sinpetru, NH Crisp, D Mostaza-Prieto… - Computer Physics …, 2022 - Elsevier
ADBSat is a novel software that determines the aerodynamic properties of any body in free-
molecular flow. Its main advantage is the fast approximation of the aerodynamics of …

Qualitative and quantitative assessment of the SET HASDM database

RJ Licata, PM Mehta, WK Tobiska, BR Bowman… - Space …, 2021 - Wiley Online Library
Abstract The High Accuracy Satellite Drag Model (HASDM) is the operational thermospheric
density model used by the US Space Force Combined Space Operations Center. By using …

[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 …