| Design and calibration of the X-33 flush airdata sensing (FADS) system S Whitmore, B Cobleigh, E Haering, Jr 36th AIAA aerospace sciences meeting and exhibit, 201, 1998 | 158 | 1998 |
| Flush airdata sensing (FADS) system calibration procedures and results for blunt forebodies B Cobleigh, S Whitmore, E Haering, Jr, J Borrer, V Roback 9th International Space Planes and Hypersonic Systems and Technologies …, 1999 | 111 | 1999 |
| High regression rate hybrid rocket fuel grains with helical port structures SA Whitmore, SD Walker, DP Merkley, M Sobbi Journal of Propulsion and Power 31 (6), 1727-1738, 2015 | 106 | 2015 |
| Comparing hydroxyl terminated polybutadiene and acrylonitrile butadiene styrene as hybrid rocket fuels SA Whitmore, ZW Peterson, SD Eilers Journal of Propulsion and Power 29 (3), 582-592, 2013 | 93 | 2013 |
| Fault-tolerant neural network algorithm for flush air data sensing TJ Rohloff, SA Whitmore, I Catton Journal of aircraft 36 (3), 541-549, 1999 | 79 | 1999 |
| Simulation of a flush air-data system for transatmospheric vehicles JC Ellsworth, SA Whitmore Journal of Spacecraft and Rockets 45 (4), 716-732, 2008 | 70 | 2008 |
| Air data sensing from surface pressure measurements using a neural network method TJ Rohloff, SA Whitmore, I Catton AIAA journal 36 (11), 2094-2101, 1998 | 67 | 1998 |
| Preliminary Results From a Subsonic High Angle-of-Attack Flush Airdata Sensing (HI-FADS) System: Design, Calibration, and Flight Test Evaluation SA Whitmore, TR Moes, TJ Larson National Aeronautics and Space Administration, Ames Research Center, Dryden …, 1990 | 60 | 1990 |
| Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack TJ Larson, SA Whitmore, LJ Ehernberger, JB Johnson, PM Siemers III NASA, 1987 | 60 | 1987 |
| Development of a power-efficient, restart-capable arc ignitor for hybrid rockets SA Whitmore, NR Inkley, DP Merkley, MI Judson Journal of Propulsion and Power 31 (6), 1739-1749, 2015 | 59 | 2015 |
| Closed-form integrator for the quaternion (Euler angle) kinematics equations SA Whitmore US Patent 6,061,611, 2000 | 59 | 2000 |
| Measurement uncertainty and feasibility study of a flush airdata system for a hypersonic flight experiment SA Whitmore, TR Moes Applied Aerodynamics Conference, 1994 | 57 | 1994 |
| Engineering model for self-pressurizing saturated-N2O-propellant feed systems SA Whitmore, SN Chandler Journal of propulsion and Power 26 (4), 706-714, 2010 | 54 | 2010 |
| In-flight demonstration of a real-time flush Airdata sensing (RT-FADS) system S Whitmore, R Davis, J Fife 20th Atmospheric Flight Mechanics Conference, 3433, 1995 | 54 | 1995 |
| Analytical and experimental comparisons of HTPB and ABS as hybrid rocket fuels S Whitmore, Z Peterson, S Eilers 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5909, 2011 | 51 | 2011 |
| Reentry air data for a sub-orbital spacecraft based on X-34 design J Ellsworth, S Whitmore 45th AIAA aerospace sciences meeting and exhibit, 1200, 2007 | 50 | 2007 |
| Development of a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system SA Whitmore SAE Aerotech 1991 Conference, 1991 | 48 | 1991 |
| Three-dimensional printing of “Green” fuels for low-cost small spacecraft propulsion systems SA Whitmore Journal of Spacecraft and Rockets 55 (1), 13-26, 2018 | 43 | 2018 |
| Engineering model for hybrid fuel regression rate amplification using helical ports SA Whitmore, SD Walker Journal of propulsion and power 33 (2), 398-407, 2017 | 43 | 2017 |
| Survey of selected additively manufactured propellants for arc ignition of hybrid rockets SA Whitmore, SL Merkley, L Tonc, SD Mathias Journal of Propulsion and Power 32 (6), 1494-1504, 2016 | 42* | 2016 |
