|
AIAA 12th Small Satellite Conference - Hydrogen Peroxide for Smaller Satellites
AIAA 13th Small Satellite Conference - Progress Toward Hydrogen Peroxide Micro-Propulsion
AIAA Responsive Space 2007 - Progress in Technology Demonstration of a Small Hybrid Launch Vehicle
Berkeley - Theoretical Analysis and Experimental Verification of Mono-Propellant Driven Free Piston Hydraulic Pump
Boeing - Non Toxic Reaction Control System - Hydrogen Peroxide - Kerosene Rocket Engine
British Interplanetary Society - High Density Liquid Rocket Boosters for Space Shuttle
Degussa - Propulse 980 Hydrogen Peroxide Enrichment System
DERA - Hydrogen Peroxide Based Propulsion System for Micro Air Vehicle Applications
Goddard - Nanosatellite Propulsion of MEMS - Hydrogen Peroxide Development
Goddard - Comparitive Study of Pumping Systems for Chemical Propulsion Altitude Test Stands
Langley - Experimental Hydrogen Peroxide Rocket System and Its Use in Meas Aileron & Rudder Effectiveness
Langley - Hydrogen Peroxide Turboject Engine Simulator Wind Tunnel Powered Model
Langley - Jet Interference Effects Model for Single Engine VSTOL Airplane Mach 0.6 to 1.0
Langley - Target Type Thrust Reverser Transonic Aerodynamic Characteristics for Single Engine Fighter Model
Lewis - Effects of Propellant and Catalyst Bed Temperature on Thrust Buildup of Hydrogen Peroxide Reaction Control Rockets
Lewis - Hovering Transition Flight of 1/5th Scale Model of Jet Powered VTOL Research Airplane
Lewis - Metalized Gelled Mono-Propellants
LLNL - Autonomous Agile Micro Satellites and Support Technology
LLNL - Autonomous Agile Micro Satellites and Support Technology for Use in LEO
LLNL - Hydrogen Peroxide for Smaller Satellites
LLNL - Hydrogen Peroxide Gas Generator Cycle with Reciprocating Pump
LLNL - Hydrogen Peroxide Storage in Small Sealed Tanks
LLNL - Lightweight Leaktight Quad Pump for Mars Access
LLNL - Mars Ascent Propulsion on Minimum Scale
LLNL - Mar Ascent Propulsion Options for Small Sample Return Vehicles
LLNL - Performance of New Lightweight Reciprocating Pump
LLNL - Progress Toward Hydrogen Peroxide Micropropulsion
LLNL - Propulsion Engineering Study for Small Scale Mars Missions
LLNL - Pump Fed Propulsion for Mars Ascent and Other Challeging Maneuvers
LLNL - Recent Developments in Hydrogen Peroxide Pumped Propulsion
LLNL - Reciprocating Pump System for Space Propulsion
LLNL - Self Pressurization HTP Feed Systems
LLNL - Single Stage to Orbit Mass Budgets Derived from Propellant Density and Isp
LLNL - Test Results for Reciprocating Pump Powered by Decomposed Hydrogen Peroxide
NACA - Hydrogen Peroxide Turbojet Engine Simulator for Wind Tunnel Powered Model
NACA - Simulated Afterburner Performance with Injection of Hydrogen Peroxide for Thrust Augmentation
NACA - Turbojet Combustor Performance with Injection of Hydrogen Peroxide for Thrust Augmentation
Sandia - Hydrogen Peroxide Based Propulsion and Power Systems
Sandia - Investigation of Hypergolic Fuels with Hydrogen Peroxide
SSC - Recent Advances in Hydrogen Peroxide Propulsion Test Capabilities at NASA Stennis Space Center
U of Maryland - Single Fluid - Life Support, Power, Propulsion and Thermal Control
USAF Academy - Design and Test of Hydrogen Peroxide MEMS Thruster
USFE - Upper Stage Flight Experiment - Hydrogen Peroxide - Kerosene Rocket Engine
WSTF - Hazard Assessment of PPE for Hydrogen Peroxide Service
Copyright (c) 2005-2010 General Kinetics Inc. All rights reserved.
email: gkllc@gkllc.com
|