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OCO-2 (Orbiting Carbon Observatory-2) on Schedule for a 01 July 2014 Launch
Study of Movement and Seepage Along Levees Using DInSAR and the UAVSAR Instrument
Command and Data Handling System for the Panchromatic Fourier Transform Spectrometer
Delta-V Budgets for Robotic and Human Exploration of Phobos and Deimos
Innovations in Delta Differential One-Way Range: from Viking to Mars Science Laboratory
Propulsive Maneuver Design for the 2007 Mars Phoenix Lander Mission
Precision Formation Delta-V Requirements for Distributed Platforms in Earth Orbit
Flight path control strategies for the 2003 Mars Exploration Rover (MER) mission
2001 Mars Odyssey orbit determination during interplanetary cruise
2001 Mars Odyssey orbit determination during interplanetary cruise
Preliminary Statistical Delta-V Analysis for a Representative Europa Orbiter Mission
Microspacecraft Secondary Payload Mission Opportunities
Measuring the Thermal Accommodation Coefficient while Aerobraking Magellan
Planetary Mission Performance for Small Solar Electric Propulsion Spacecraft
Hypersonic performance of several basic and modified diamond cross-section delta wing configurations
Further experimental investigations of delta and double-delta wing flow fields at low speeds
Lunar orbit mission analysis for the improved Delta launch vehicle and AIMP-D SPACECRAFT
Aerodynamic effect of volume addition to a high L/D wing/body at Mach 6.0.
Performance of X 258 third-stage motor on Delta 36 /OT-3/
A study of pressure and heat transfer over an 80 deg sweep slab delta wing in hypersonic flow
GT-2 flight test data. Book XII - Timing, pressure and altitude comparisons
Application of Airbreathing Propulsion to Reusable Launch Vehicles
Flight investigation of the aerodynamic properties of an Ogee wing
Nasas syncom c satellite is set for launching news release no. 64-193
Nasa to launch another relay communications satellite news release 64-9
A Critical Study of Delta-Wing Configurations for the Supersonic Transport Application
A CRITICAL STUDY OF DELTA-WING CONFIGURATIONS FOR THE SUPERSONIC TRANSPORT APPLICATION