Journal of Spacecraft and Rockets
Overview
publication venue for

General Dynamics for Single and DualAxis Rotating Rigid Spacecraft Components
2024

Investigation of SurfaceCatalycity Effects on Hypersonic Glide Vehicle Trajectory Optimization
2024

SingleAgent Reinforcement Learning for Scalable EarthObserving Satellite Constellation Operations
2024

CoDelivery of a Martian Probe Network
2023

Passively Safe Spacecraft Motion Using Reachable Sets and Orbital Element Differences
2023

Relative Motion in the Velocity Frame for Atmospheric Entry Trajectories
2023

Atmospheric Density Estimation Techniques for Aerocapture
2023

Designing LowThrust Transfers near EarthMoon L_{2} via MultiObjective Reinforcement Learning
2023

Touchless Potential Sensing of Differentially Charged Spacecraft Using XRays
2023

Methods to Detect ImpactInduced Orbit Perturbations Using Spacecraft Navigation Data
2023

Decentralized Formation and Constellation Stability Design Requirements Using Differential Mean Orbit Elements
2022

Remote Electrostatic Potential Sensing for Proximity Operations: Comparison and Fusion of Methods
2022

Touchless Potential Sensing of Differentially Charged Spacecraft Using Secondary Electrons
2022

Constrained Attitude Maneuvering via Modified Rodrigues Parameters Based Motion Planning Algorithms
2022

Constrained Guidance for Spacecraft Proximity Operations Under Electrostatic Perturbations
2022

Using PlasmaInduced XRay Emission to Estimate Electrostatic Potentials on Nearby Space Objects
2022

Assessment of Hypersonic DoubleCone Experiments for Validation of Thermochemistry Models
2022

Deployment Dynamics Analysis of an OrigamiFolded Spacecraft Structure with Elastic Hinges
2022

Effects of Electric Potential Uncertainty on Electrostatic Tractor Relative Motion Control Equilibria
2022

Generation of Spacecraft Operations Procedures Using Deep Reinforcement Learning
2022

Optimal Information Filtering for Robust Aerocapture Trajectory Generation and Guidance
2022

Diamagnetically Enhanced Electrolysis and Phase Separation in Low Gravity
2022

Extendable Origami Multilayer Insulation Design and Thermal Performance Characterization (Jan, 10.2514/1.A34883, 2021)
2022

Flight Mechanics Feasibility Assessment for CoDelivery of DirectEntry Probe and Aerocapture Orbiter
2022

MultiEvent Jettison Guidance Approaches for DragModulation Aerocapture
2022

Quantifying Uncertainty in Predictions of Spacecraft Erosion Induced by a Hall Thruster
2021

Simulation and Uncertainty Quantification of Electron Beams in Active Spacecraft Charging Scenarios
2021

Landing Site Selection Using a Geometrically Conforming Footprint on Hazardous Small Bodies
2021

ElectronBased Touchless Potential Sensing of Shape Primitives and DifferentiallyCharged Spacecraft
2021

Designing LowThrust Transfers to HighInclination Science Orbits via Hybrid Optimization
2021

Centroid and Apparent Diameter Optical Navigation on Mars Orbit
2021

Cislunar Periodic Orbit Analysis for Persistent Space Object Detection Capability
2021

Extendable Origami Multilayer Insulation Design and Thermal Performance Characterization
2021

Global Steering for Control Moment Gyroscope Clusters Using Heuristic Variable Search Techniques
2021

Effect of N Atoms on OAtom Reactivity with Carbon
2021

Lyapunov Optimal Touchless Electrostatic Detumbling of Space Debris in GEO Using a Surface Multisphere Model
2021

Attitude Estimation with Albedo Interference on Sun Sensor Measurements
2021

Chip Scale Atomic ClockDriven OneWay Radiometric Tracking for LowEarthOrbit CubeSat Navigation
2021

Evidence for Drag Coefficient Modeling Errors near and Above the OxygentoHelium Transition
2020

IonicLiquidBased Contactors for Carbon Dioxide Removal from Simulated Spacecraft Cabin Atmospheres
2020

Removing Rate Unobservability in SunHeading Filters Without Rate Gyroscopes
2020

Improved Modal Damping Characterization for SmallScale Heliogyro Blades
2020

Active Mass Ejection for Asteroid Manipulation and Deflection
2020

Development of an Achievability Propellant Limit Algorithm for a Piloted, Lunar Lander
2020

Prospects of a Hybrid Magnetic/Electrostatic Sample Container Retriever
2020

Multisphere Method for Flexible Conducting Space Objects: Modeling and Experiments
2020

Arcjet Thruster Influence on Local Magnetic Field Measurements from a Geostationary Satellite
2020

Simulation of Nonspherical Asteroid Landers: Contact Modeling and Shape Effects on Bouncing
2020

Conjugate Analyses of Ablation in Rocket Nozzles
2019

Heterogeneous Surface Multisphere Models Using Method of Moments Foundations
2019

Orbital Stability Regions for Hypothetical Natural Satellites of (101955) Bennu
2019

General Hinged RigidBody Dynamics Approximating FirstOrder Spacecraft Solar Panel Flexing
2018

Robust Attitude Control Using a DoubleGimbal VariableSpeed Control Moment Gyroscope
2018

Prearrival Deployment Analysis of Rovers on Hayabusa2 Asteroid Explorer
2018

Conceptual Design of an AirBreathing Electric Thruster for CubeSat Applications
2018

Convex Optimization for Power Tracking of DoubleGimbal VariableSpeed Control Moment Gyroscopes
2018

Modeling Magnetohydrodynamic Energy Generation and Storage in Planetary Entry System Conceptual Design
2018

Parametric Study of Ballistic Lander Deployment to Small Bodies
2017

Unsteady Simulations of Rocket Plume Expansions in Geostationary Earth Orbit
2017

SteadyState Attitude and Control Effort Sensitivity Analysis of Discretized Thruster Implementations
2017

Thermal Vacuum Evaluation of Simulated Spacecraft Radiators with Discretized Emissivity Surface Properties
2017

TwoDimensional Modeling of Ablation and Pyrolysis with Application to Rocket Nozzles
2017

Comparative Analysis of Satellite Aerodynamics and Its Application to SpaceObject Identification
2016

Miniature XRay Solar Spectrometer: A ScienceOriented, University 3U CubeSat
2016

Characterizing a Transient Heat Flux Envelope for LunarSurface Spacesuit Thermal Control Applications
2015

Computation of Hypersonic Flows Using the Direct Simulation Monte Carlo Method
2015

Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation
2015

Contact Motion on Surface of Asteroid
2014

Jovian Capture of a Spacecraft with a SelfBalanced Electrodynamic Bare Tether
2014

Nonlinear Dynamics of Objects in Transition Flow During Atmospheric Entry
2014

Investigations of Peripheral Propulsive Deceleration Jets on a Mars Science Laboratory Aeroshell
2014

Human Spatial Orientation Perception During Simulated Lunar Landing Motions
2014

RigidBody Dynamics in FreeMolecular and Transition Flow
2014

Aerodynamic Analysis Based on Challenging Minisatellite Payload Satellite LifttoDrag Measurements
2013

Effect of Density Model TimeDelay Errors on Orbit Prediction
2013

Propulsion Deceleration Studies Using Planar LaserInduced Iodine Fluorescence and Computational Fluid Dynamics
2013

Characterizing Human Spacecraft Safety and Operability Through a Minimum Functionality Design Methodology
2013

SemiEmpirical Satellite Accommodation Model for Spherical and Randomly Tumbling Objects
2013

Hypersonic Flow and Radiation Analysis of the Automated Transfer Vehicle Jules Verne
2013

Effectiveness of a Magnetohydrodynamics System for Mars Entry
2012

Effectiveness of a Magnetohydrodynamics System for Mars Entry
2012

Tethered Coulomb Structure Applied to Close Proximity Situational Awareness
2012

Sequential Orbit Determination with the CubedSphere Gravity Model
2012

Attitude and Power Analysis of TwoNode Multitetheral Coulomb Structures
2011

Interactions of SingleNozzle Sonic Propulsive Deceleration Jets on Mars Entry Aeroshells
2011

Rotational Stiffness Study of TwoElement Tethered Coulomb Structures
2011

Drag Coefficients of Satellites with Concave Geometries: Comparing Models and Observations
2011

Modeling of Stardust Entry at High Altitude, Part 2: Radiation Analysis
2010

Semiempirical Model for Satellite EnergyAccommodation Coefficients
2010

Modeling of Stardust Entry at High Altitude, Part 1: Flowfield Analysis
2010

Numerical Study of Magnetoaerodynamic Flow Around a Hemisphere
2010

Modeling of Electromagnetic Manipulation of Plasmas for Communication During Reentry Flight
2010

Coning Control of Solar Sails Using Magnetic Momentum Error Reduction
2009

Sensitivity of Orbit Predictions to Density Variability
2009

Numerical Study of PlasmaAssisted Aerodynamic Control for Hypersonic Vehicles
2009

Analysis of an Electromagnetic Mitigation Scheme for Reentry Telemetry Through Plasma
2008

Comment on Special Section: New Perspectives on the Satellite Drag Environments of Earth, Mars, and Venus Reply
2008

Multiscale ParticleContinuum Simulations of Hypersonic Flow over a Planetary Probe
2008

Improved Atomic Oxygen Quantification Within the Earth's Upper Atmosphere Through Numerical Corrections
2008

Electromagnetic reduction of plasma density during atmospheric reentry and hypersonic flights
2008

Collisionless gas expanding into vacuum
2007

Density and winds in the thermosphere deduced from accelerometer data
2007

Introduction: New perspectives on the satellite drag environments of Earth, Mars, and Venus
2007

Satellite drag variability at Earth, Mars, and Venus due to solar rotation
2007

Stormtime equatorial density enhancements observed by CHAMP and GRACE
2007

Finite Element Modeling of Sail Deformation Under Solar Radiation Pressure
2007

Theoretical and numerical study of freemolecular flow problems
2007

Erratum on simulation of aerodynamic influences on rocketmounted oxygen sensors (vol 43, pg 1387, 2006)
2007

Automated operational orbit determination for the Ice Cloud and Land Elevation Satellite mission
2006

Distributed and localized active vibration isolation in membrane structures
2006

Maximizing payload mass fractions of spacecraft for interplanetary electric propulsion missions
2006

Applying analysis of international space station crewtime utilization to mission design
2006

Computational Analysis of HighAltitude Ionization Gauge Flight Measurements
2006

Dynamic wrinkle reduction strategies for cablesuspended membrane structures
2005

Estimating parameterized postNewtonian parameters from spacecraft radiometric tracking data
2005

Generalized model for solar
2005

Solarsystem escape trajectories using solar sails
2004

Energy accommodation in hyperthermal gassurface collisions: Aerobraking in planetary atmospheres
2004

Orbit determination for the QuikSCAT spacecraft
2002

Development of a target marker for landing on asteroids
2001

Interactions between spacecraft and thruster plumes
2001

Review of Hall thruster plume modeling
2001

Wearfield measurement and modeling results for flighttype arcjet: Hydrogen atom
2001

Solar sail orbit operations at asteroids
2001

Nearfield measurement and modeling results for flighttype arcjet: NH molecule
2001

Modeling of a pulsed plasma thruster from plasma generation to plume far field
2000

Particle simulations of a Hall thruster plume
2000

Detailed simulation of surface chemistry leading to spacecraft glow
1999

Detailed computation of ultraviolet spectra in rarefied hypersonic flow
1998

Precision orbit determination for the GEOSAT FollowOn satellites
1998

Chargedparticle telescope experiment on Clementine
1995

PARTICLE SIMULATIONS OF HELIUM MICROTHRUSTER FLOWS
1994

NONLINEAR DYNAMIC PHENOMENA IN THE SPACESHUTTLE THERMAL PROTECTION SYSTEM
1982

Constrained Attitude Maneuvering via ModifiedRodriguesParameterBased Motion Planning Algorithms
2021

Impact of Electrostatic Perturbations on Proximity Operations in High Earth Orbits
2020

Electrostatic Tractor Analysis Using a Measured Flux Model
2020

Rapid Modeling of Electrostatic Forces and Torques Considering Dielectrics
2019

Active Mass Ejection for Asteroid Manipulation and Deflection
2019

Numerical Investigation of Multinozzle Propulsive Deceleration Jets for Mars Entry Aeroshells
2011

Estimation and Modeling of Enceladus Plume Jet Density Using Cassini Flight Data
2010

Comparison of TIMED satellite drag with solar EUV experiment (SEE) measurements
2006

Simulation of aerodynamic influences on rocketmounted oxygen sensors
2005

Direct simulation Monte Carlo investigation of hyperthermal oxygen beam exposures
2004

Erosion of KaptonĀ® H by hyperthermal atomic oxygen
2004

Homogeneous silica formed by the oxidation of Si(100) in hyperthermal atomic oxygen
2004
Research
keywords

0901 Aerospace Engineering, 0913 Mechanical Engineering