Stephen A. Whitmore

发表

High angle-of-attack flush airdata sensing system

Stephen A. Whitmore, T. J. Larson, Timothy R. Moes, 1992 .

Design of a Flush Airdata System (FADS) for the Hypersonic Air Launched Option (HALO) Vehicle

Stephen A. Whitmore, Timothy R. Moes, Dwain A. Deets, 1994 .

Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack

Stephen A. Whitmore, Terry J. Larson, L. J. Ehernberger, 1987 .

Sounding Rocket Energy Management Using Cold-Gas Aerospike Thrusters

Stephen A. Whitmore, Andrew Bath, Nathan Erni, 2011 .

Development and Testing of a Green-Propellant Micro-Hybrid Thruster with Electrostatic Ignition

Stephen A. Whitmore, Michael D. Judson, 2012 .

High Regression Rate Hybrid Rocket Fuel Grains with Helical Port Structures

Stephen A. Whitmore, Mansour Sobbi, Sean D. Walker, 2014 .

An Optimal Deconvolution Method for Reconstructing Pneumatically Distorted Near-Field Sonic Boom Pressure Measurements

Stephen A. Whitmore, L. J. Ehernberger, Edward A. Haering, 2013 .

Launch and Deployment Analysis for a Small, MEO, Technology Demonstration Satellite

Stephen A. Whitmore, Tyson K. Smith, 2008 .

Measurements of the Basic SR-71 Airplane Near-Field Signature

Stephen A. Whitmore, L. J. Ehernberger, Edward A. Haering, 1999 .

FORTRAN program for analyzing ground-based radar data: Usage and derivations, version 6.2

Stephen A. Whitmore, Edward A. Haering, 1995 .

Launch and Deployment of the High-Latitude Dynamic E-Field (HiDEF) Explorer Satellite Constellation

Stephen A. Whitmore, Bryan Bingham, Quinn Young, 2008 .

Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic Mach numbers

Stephen A. Whitmore, Timothy R. Moes, Frank L. Jordan, 1993 .

Design of a Passively Reefed, Collapsible Drogue Parachute System

Stephen A. Whitmore, Elsa J. Hennings, 2007 .

Direct-Entry, Aerobraking, and Lifting Aerocapture for Human-Rated Lunar Return Vehicles

Stephen A. Whitmore, Daniel W. Banks, Benjamin M. Andersen, 2006 .

In-flight demonstration of a Real-Time Flush Airdata Sensing (RT-FADS) system

Stephen A. Whitmore, R. J. Davis, John Michael Fife, 1995 .

Novel Technique for Reconstructing High-Frequency Transient Rocket Chamber-Pressure Measurements

Stephen A. Whitmore, Matthew D. Wilson, Shannon D. Eilers, 2010 .

Leveraging Utah State's Experimental Rocketry Program for a Senior-design Capstone Course

Stephen A. Whitmore, Shannon D. Eilers, S. Whitmore, 2009 .

Design and Calibration of the X-33 Flush Airdata Sensing (FADS) System

Stephen A. Whitmore, Edward A. Haering, Brent R. Cobleigh, 1998 .

Three-Dimensional Printing of “Green” Fuels for Low-Cost Small Spacecraft Propulsion Systems

Stephen A. Whitmore, 2017 .

Design of a Small Scale Aerospike Nozzle and Associated Testing Infrastructure for Experimental Evaluation of Aerodynamic Thrust Vectoring

Stephen A. Whitmore, Matthew D. Wilson, Shannon D. Eilers, 2010 .

Preliminary results from a subsonic high-angle-of-attack flush airdata sensing (HI-FADS) system - Design, calibration, algorithm development, and flight test evaluation

Stephen A. Whitmore, Timothy R. Moes, Terry J. Larson, 1990 .

A Base Drag Reduction Experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) Flight Program

Stephen A. Whitmore, Timothy R. Moes, 1999 .

Design and Testing of FDM Manufactured Paraffin-ABS Hybrid Rocket Motors

Stephen A. Whitmore, Andrew Bath, Jonathan McCulley, 2012 .

Transient Thrust Model for a Small Scale Self-Pressured Hybrid Rocket Motor

Stephen A. Whitmore, Spencer N. Chandler, 2009 .

Air data position-error calibration using state reconstruction techniques

Stephen A. Whitmore, Terry J. Larson, L. J. Ehernberger, 1984 .

Development and Flight Testing of Energy Management Algorithms for Small-Scale SoundingRockets

Stephen A. Whitmore, Shane B. Robinson, Shannon D. Eilers, 2009 .

Real-gas extensions to tangent-wedge and tangent-cone analysis methods

Stephen A. Whitmore, 2007 .

Development and Testing of a Multiple Use Plug Hybrid (for) Nanosats (MUPHyN)

Stephen A. Whitmore, Shannon D. Eilers, 2012 .

Interim Access to the International Space Station Using Evolved Expendable Launch Vehicles

Stephen A. Whitmore, Tyson K. Smith, 2010 .

Application of a flush airdata sensing system to a wing leading edge (LE-FADS)

Stephen A. Whitmore, Timothy R. Moes, Mark W. Czerniejewski, 1993 .

The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system

Stephen A. Whitmore, Timothy R. Moes, 1991 .

Air Data Sensing from Surface Pressure Measurements Using a Neural Network Method

Stephen A. Whitmore, Ivan Catton, Thomas J. Rohloff, 1998 .

Side Force Amplification on an Aerodynamically Thrust Vectored Aerospike Nozzle

Stephen A. Whitmore, Matthew D. Wilson, Shannon D. Eilers, 2011 .

Parametric Study of Biconic Re-Entry Vehicles

Stephen A. Whitmore, Daniel W. Banks, Bryan Steele, 2007 .

Flush Airdata Sensing (FADS) System Calibration Procedures and Results for Blunt Forebodies

Stephen A. Whitmore, Edward A. Haering, Brent R. Cobleigh, 1999 .

Design of In-Flight Instrumentation to Characterize a Hybrid Thruster

Stephen A. Whitmore, Cameron Turner, Andrew Young, 2017 .

Development and Testing of a Drogue Parachute System for X-37 Altv/B-52h Separation

Stephen A. Whitmore, Elsa J. Hennings, Brent R. Cobleigh, 2013 .

Preliminary results from a subsonic high angle-of-attack flush airdata sensing (HI-FADS) system: Design, calibration, and flight test evaluation

Stephen A. Whitmore, Timothy R. Moes, Terry J. Larson, 1990 .

Experimental characterization of the effects of pneumatic tubing on unsteady pressure measurements

Stephen A. Whitmore, Robert E. Curry, Glenn B. Gilyard, 1990 .

Engineering Model for Self-Pressurizing Saturated-N2O-Propellant Feed Systems

Stephen A. Whitmore, Spencer N. Chandler, 2010 .

Base-Drag-Reduction Experiments on the X-33 Linear Aerospike SR-71 Flight Program

Stephen A. Whitmore, Timothy R. Moes, 2000 .

Closed-Loop Precision Throttling of a Hybrid Rocket Motor

Stephen A. Whitmore, Shannon D. Eilers, Zachary W. Peterson, 2014 .

Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flight

Stephen A. Whitmore, Timothy R. Moes, 1991 .

A Low-cost Trajectory Estimation System for Drones and Rockets

Stephen A. Whitmore, Tyler J. Gardner, 2019 .

Pneumatic distortion compensation for aircraft surface pressure sensing devices

Stephen A. Whitmore, Cornelius T. Leondes, 1991 .

Large Constellation Development using Small Satellites

Stephen A. Whitmore, Bryan Bingham, Quinn Young, 2008 .

Closed-Loop Thrust and Pressure Profile Throttling of a Nitrous-Oxide HTPB Hybrid Rocket Motor

Stephen A. Whitmore, Shannon D. Eilers, Zachary W. Peterson, 2012 .

Additive manufacturing as an enabling technology for "green" hybrid spacecraft propulsion

Stephen A. Whitmore, 2015, 2015 7th International Conference on Recent Advances in Space Technologies (RAST).

Fault-Tolerant Neural Network Algorithm for Flush Air Data Sensing

Stephen A. Whitmore, Ivan Catton, Thomas J. Rohloff, 1999 .

Preliminary airborne measurements for the SR-71 sonic boom propagation experiment

Stephen A. Whitmore, L. J. Ehernberger, Edward A. Haering, 1995 .

A preliminary look at techniques used to obtain airdata from flight at high angles of attack

Stephen A. Whitmore, Timothy R. Moes, 1990 .

Measurement uncertainty and feasibility study of a flush airdata system for a hypersonic flight experiment

Stephen A. Whitmore, Timothy R. Moes, 1994 .

Launch and Deployment Analysis for a Small, Medium Earth Orbit, Technology-Demonstration Satellite

Stephen A. Whitmore, Tyson K. Smith, 2009 .

Development of a pneumatic high-angle-of-attack flush airdata sensing system

Stephen A. Whitmore, S. Whitmore, 1991 .

Consumable Spacecraft Structures with Integrated, 3-D Printed ABS Thrusters

Stephen A. Whitmore, 2017 .

Reentry Air Data for a Sub-orbital Spacecraft Based on X-34 Design

Stephen A. Whitmore, Joel C. Ellsworth, 2007 .

Failure detection and fault management techniques for flush airdata sensing systems

Stephen A. Whitmore, Cornelius T. Leondes, Timothy R. Moes, 1992 .

Effects of Radiation Heating on Additively Printed Hybrid Fuel Grain O/F Shift

Stephen A. Whitmore, Stephen L. Merkley, 2016 .

Development and Testing of a Green Monopropellant Ignition System

Stephen A. Whitmore, Terry L. Taylor, Shannon D. Eilers, 2013 .

A Survey of Additively Manufactured Propellant Materials for Arc-Ignition of Hybrid Rockets

Stephen A. Whitmore, John D. DeSain, Jerome K. Fuller, 2015 .

Effects of Radiation Heating on Additively Printed Hybrid Fuel Grain Oxidizer-To-Fuel Ratio Shift

Stephen A. Whitmore, Stephen L. Merkley, S. Whitmore, 2016 .

Development and Testing of Three Alternative Designs for Additively Manufactured Hybrid Thrusters

Stephen A. Whitmore, S. Whitmore, Spencer Mathias, 2016 .

Drag Reduction on Blunt-Based Vehicles Using Forebody Surface Roughness

Stephen A. Whitmore, Jonathan W. Naughton, 2002 .

Maneuvering and Gravity Offset Flight Controls for an Extraterrestrial Surface Landing Research Vehicle

Stephen A. Whitmore, M. Ryan Schaefermeyer, M. Schäfermeyer, 2010 .

Hydrocarbon-Seeded Ignition System for Small Spacecraft Thrusters Using Ionic Liquid Propellants

Stephen A. Whitmore, Terry L. Taylor, Shannon D. Eilers, 2013 .

Experimental Investigation of Base-Drag Reduction via Boundary-Layer Modification

Stephen A. Whitmore, Jonathan W. Naughton, Vibhav Durgesh, 2013 .

Correlation of Hybrid Rocket Propellant Regression Measurements with Enthalpy-Balance Model Predictions

Stephen A. Whitmore, Shannon D. Eilers, S. Whitmore, 2007 .

Development of a Pneumatic High-Angle-of-Attack Flush Airdata Sensing (HI-FADS) System

Stephen A. Whitmore, S. Whitmore, 2022 .

Comparing Hydroxyl Terminated Polybutadiene and Acrylonitrile Butadiene Styrene as Hybrid Rocket Fuels

Stephen A. Whitmore, Shannon D. Eilers, Zachary W. Peterson, 2013 .

Engineering Model for Hybrid Fuel Regression Rate Amplification Using Helical Ports

Stephen A. Whitmore, Sean D. Walker, S. Whitmore, 2017 .

Analytical and Experimental Evaluation of Aerodynamic Thrust Vectoring on an Aerospike Nozzle

Stephen A. Whitmore, Shannon D. Eilers, Zachary W. Peterson, 2010 .

Side-Force Amplification on an Aerodynamically Thrust-Vectored Aerospike Nozzle

Stephen A. Whitmore, Shannon D. Eilers, Zachary W. Peterson, 2012 .

Wind-Tunnel Investigations of Blunt-Body Drag Reduction Using Forebody Surface Roughness

Stephen A. Whitmore, Jonathan W. Naughton, Robert E. Curry, 2001 .

Development of a Power Efficient, Restart-Capable Arc Ignitor for Hybrid Rockets

Stephen A. Whitmore, Daniel P. Merkley, S. Whitmore, 2014 .

Simulation of a Flush Air-Data System for Transatmospheric Vehicles

Stephen A. Whitmore, Joel C. Ellsworth, S. Whitmore, 2008 .

Dynamic Response of Pressure Sensing Systems in Slip-Flow with Temperature Gradients

Stephen A. Whitmore, S. Whitmore, Brian J. Petersen, 1999 .

Analytical and Experimental Comparisons of HTPB and ABS as Hybrid Rocket Fuels

Stephen A. Whitmore, Shannon D. Eilers, Zachary W. Peterson, 2011 .

Frequency Response of Pressure Sensor Configurations in Slip-Flow Conditions

Stephen A. Whitmore, S. Whitmore, 2002 .

Formulaton of a general technique for predicting pneumatic attenuation errors in airborne pressure sensing devices

Stephen A. Whitmore, 1988 .

Additively Manufactured Acrylonitrile-Butadiene-Styrene–Nitrous-Oxide Hybrid Rocket Motor with Electrostatic Igniter

Stephen A. Whitmore, S. Whitmore, 2015 .

A Novel Technique for Reconstructing High-Frequency Transient Rocket Chamber Pressure Measurements

Stephen A. Whitmore, Shannon D. Eilers, S. Whitmore, 2009 .

Frequency Response Model for Branched Pneumatic Sensing Systems

Stephen A. Whitmore, S. Whitmore, 2006 .

Engineering Model of Temperature-Induced Pneumatic Sensor Pressure Gradients for Rarefied Flow Conditions

Stephen A. Whitmore, S. Whitmore, 2008 .

Survey of Selected Additively Manufactured Propellants for Arc Ignition of Hybrid Rockets

Stephen A. Whitmore, Stephen L. Merkley, S. Whitmore, 2016 .

Formulation and implementation of a practical algorithm for non-stationary adaptive state estimation

Stephen A. Whitmore, Cornelius T. Leondes, 1986 .

In-flight demonstration of a real-time flush airdata sensing system

Stephen A. Whitmore, R. J. Davis, John Michael Fife, 1996 .

Modification of Base Drag through Boundary-Layer Manipulation

Stephen A. Whitmore, Jonathan W. Naughton, Robert K. Decker, 2002 .

A Dynamic Response Model for Pressure Sensors in Continuum and High Knudsen Number Flows with Large Temperature Gradients

Stephen A. Whitmore, Brian J. Petersen, David D. Scott, 1996 .

Wiener Deconvolution for Reconstruction of Pneumatically Attenuated Pressure Signals

Stephen A. Whitmore, S. Whitmore, Matthew D. Wilson, 2011 .

Engineering Model for Hybrid Rocket Regression Rate Amplification by Helical Fuel Ports.

Stephen A. Whitmore, Sean D. Walker, Logan Utah, 2015 .

Development of a Power-Efficient, Restart-Capable Arc Ignitor for Hybrid Rockets

Stephen A. Whitmore, Michael I. Judson, Daniel P. Merkley, 2015 .

Correlation of Hybrid Rocket Propellant Regression Measurements with Enthalpy-Balance Model Predictions

Stephen A. Whitmore, Shannon D. Eilers, 2007 .