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1 Operational Requirements to Air Independent Propulsion (AIP); Relating operational requirements to technical parameters for AIP
article 2005    
Author: Fitski, H.J. · Noordkamp, H.W. · Vermeulen, J.F.J.
Keywords: Defence · AIP · Batteries · Operational · Requirements · Propulsion · Walrus class submarines
[Abstract]

2 Technology status of HNF-based monopropellants for satellite propulsion
article 2004    
Author: Marée, A.G.M. · Moerel, J.L.P.A. · Weiland-Veltmans, W.H.M. · Wierkx, F.J.M. · Zevenbergen, J.
Keywords: Crystallization · Hydrazine · Oxidation · Satellites · Sensitivity analysis · Single crystals · Spacecraft propulsion · Toxicity · Vapors · Viscosity · HNF-based monopropellants · Non-toxic monopropellants · Satellite propulsion · Storage density · Propellants
[Abstract]

3 Design and development of a propulsion system for a cubesat - Based on solid propellant cool gas generator technology
article 2006    
Author: Rackemann, N.J. · Sanders, H.M. · Vliet, L.D. van
Keywords: Gas generators · Mathematical models · Orbits · Solid propellants · Cool gas generator technology · Cubesat · Orbit maneuvering · Spacecraft propulsion
[Abstract]

4 Development status of the ignition system for Vinci
article 2002    
Author: Frenken, G. · Vermeulen, E. · Bouquet, F. · Sanders, H.M.
Keywords: Aviation · Development status · Feed systems · Upper stages · Engines · Propulsion · Ignition systems · Space · Information Society
[Abstract]

5 Improvements on cool gas generators and their application in space propulsion systems
article 2014    
Author: Sanders, H.M. · Schuurbiers, C.A.H. · Vandeberg, R.J.
Keywords: Aviation · Space propulsion · Fluid Mechanics Chemistry & Energetics · EM - Energetic Materials · TS - Technical Sciences
[Abstract]

6 Cool gas micropropulsion system for cubesats
article 2009    
Author: Breukelen, E. van · Sanders, B.H. · Schuurbiers, C.A.H.
Keywords: Aviation · Basic systems · Commercial off-the-shelf systems · Cubesat · Flexible system · Flight demonstration · Maneuvering capability · Micro propulsion system · Micro-propulsion systems · Microsatellites · Nanosatellite · Netherlands · Nitrogen propellant · On orbit · Plug-and-play · Propulsion system · Qualification model · Standard module · Standardized interfaces · System description · Gas generators · Philosophical aspects · Propellants · Spacecraft propulsion · Gases
[Abstract]

7 A modular ducted rocket missile model for threat and performance assessment
article 2005    
Author: Mayer, A.E.H.J. · Halswijk, W.H.C. · Komduur, H.J. · Lauzon, M. · Stowe, R.A.
Keywords: Defence · Aircraft propulsion · Guns (armament) · Missiles · Air breathing missiles · DRCORE · Rocket missile model · Rockets
[Abstract]

8 Industrial benefits of applying HNF in monopropellant satellite propulsion
article 2001    
Author: Fick, M. · Schiebener, P. · Moerel, J.L.P.A. · Berg, R.P. van den · Sanders, H.M. · Welland-Veltmans, W.H.M.
Keywords: Aircraft fueling · Ammonium compounds · Catalyst activity · Catapults (aircraft launchers) · Decomposition · Environmental protection · Gas generators · Hydrogen peroxide · Potential energy · Satellites · Space research · Spacecraft propulsion · Stainless steel · Storage (materials) · Toxic materials · Toxicity · Earth-orbiting satellites · Satellite propulsion · Toxic fumes · Solid propellants
[Abstract]

9 Non-toxic liquid propellant selection method a requirement-oriented approach
article 2005    
Author: Bombelli, V. · Maree, A.G.M. · Caramelli, F.
Keywords: Ballistics · Commercial pressure · In-orbit · Mission objectives · Multiple use · Non-toxic alternatives · Propulsion system · Selection criteria · Selection methods · SPACE system · Technical requirement · Time frame · Time-scales · Toxic liquids · Land use · Liquid propellants · Spacecraft · Toxic materials · Spacecraft propulsion
[Abstract]

10 Green propellant propulsion concepts for space transportation and technology development needs
article 2004    
Author: Haeseler, D. · Bombelli, V. · Vuillermoz, P. · Lo, R. · Maree, A.G.M. · Caramelli, F.
Keywords: Costs · Propellants · Propulsion · Technology transfer · Thrust reversal · Toxicity · Vapors · Green propellants · Non-toxic fluids · Pollutant impact · Space transporation · Space applications
[Abstract]

11 Proof-of-principle experiment of a shock-induced combustion ramjet
article 2010    
Author: Veraar, R.G. · Mayer, A.E.H.J. · Verreault, J. · Stowe, R.A. · Farinaccio, R. · Harris, P.G.
Keywords: Weapon systems · Air flow · Axisymmetric · Boundary-layer separation · Density change · Dual cones · Free jets · Fuel-air mixtures · Heat loads · Hypersonic propulsion systems · Inviscid flows · Local heat · Mass flow rate · Oblique shock waves · Premature ignition · Proof-of-principle experiments · Ramjets · Scramjet propulsion · Shadowgraph technique · Shock induced combustion · Test object · Thermo-mechanical analysis · Air · Boundary layers · Combustors · Dynamic mechanical analysis · Flow fields · Hydrogen · Nozzles · Shock waves · Spacecraft propulsion · Testing · Thermal expansion · Thermal load · Thermocouples · Ignition
[PDF] [Abstract]

12 Proof-of-principle experiment of a shock-induced combustion ramjet
article 2009    
Author: Veraar, R.G. · Mayer, A.E.H.J. · Verreault, J. · Stowe, R.A. · Farinaccio, R. · Harris, P.G.
Keywords: Weapon systems · Air flow · Axisymmetric · Boundary-layer separation · Density change · Dual cones · Free jets · Fuel-air mixtures · Heat loads · Hypersonic propulsion systems · Inviscid flows · Local heat · Mass flow rate · Oblique shock waves · Premature ignition · Proof-of-principle experiments · Ramjets · Scramjet propulsion · Shadowgraph technique · Shock induced combustion · Test object · Thermo-mechanical analysis · Air · Boundary layers · Combustors · Dynamic mechanical analysis · Flow fields · Hydrogen · Nozzles · Shock waves · Spacecraft propulsion · Testing · Thermal expansion · Thermal load · Thermocouples · Ignition
[Abstract]

13 Modelling of composite propellant properties
article 2000    
Author: Keizers, H.L.J. · Hordijk, A.C. · Vliet, L.D. van · Bouquet, F.
Keywords: Composite propellants · Design of experiments · Propulsion · Binder systems · Cost effective · Design tradeoff · Development programmes · Model use · Propellant ingredient · Semi-empirical · Solid particles · Propellants
[Abstract]

14 Test methods for evaluating energy consumption and emissions of vehicles with electric, hybrid and fuel cell power trains
article 2000    
Author: Smokers, R.T.M. · Ploumen, S. · Conte, M. · Buning, L. · Meier-Engel, K.
Keywords: Energy consumption · Vehicle emissions · Simulations · Test procedures · Electric power trains · Hybrid power trains · Fuel cell power trains · Fuel cells · Propulsion systems
[Abstract]

15 Development of hydrazinium nitroformate based solid propellants
article 1995    
Author: Schöyer, H.F.R. · Schnorhk, A.J. · Korting, P.A.O.G. · Lit, P.J. van · Mul, J.M. · Gadiot, G. · Meulenbrugge, J.J.
Keywords: Explosives · Pilot plants · Propellants · Propulsion · Solid propellants · Composite solid propellant · Development phasis · Energetic binder · Explosive properties · Friction sensitivities · Handling characteristics · Hydrazinium nitroformate · Initial development · Composite propellants
[Abstract]

16 Particle size distribution effect on burn rate of ammonium nitrate based propellant
article 1995    
Author: Miedema, J.R. · Klein, A.J.J. · Zee, F.W.M.
Keywords: Light transmission · Nitrates · Particle size · Propellants · Propulsion · Size distribution · Ammonium nitrate · Burn rates · Different particle sizes · Pressure exponents · Specific surface area (SSA) · Temperature sensitivity · Particle size analysis
[Abstract]

17 Fuel pyrolysis effects on hybrid rocket and solid fuel ramjet combustor performance
dissertation 1991    
Author: Wilde, J.P. de
Keywords: Pyrolysis · Hybrid propulsion · Ramjet engines · Combustion · Compositions · Temperature · Solid rocket propellants · Velocity · Burning rate · Mathematical models · Reaction kinetics · Thermal degradation · Combustion chambers

18 Feasibility study for the development of a pyro starter
article 2009    
Author: Hong, M. · Welland, W. · Bouquet, F. · Lee, S.Y.
Keywords: Ballistics · Combustion gas · Concept designs · Critical design parameters · Engine start · Feasibility studies · Flame temperatures · Further development · Launch vehicle · Power turbines · Pressurized gas · Propulsion system · Turbo pumps · Combustion · Decision making · Design · Launch vehicles · Launching · Liquid propellants · Planning · Resource allocation · Spacecraft propulsion · Turbines · Starters
[Abstract]

19 Sustained combustion limits of a central dump solid fuel ramjet combustor at high altitude operational conditions
article 2018    
Author: Veraar, R.G. · Wieling, W.P.W.
Keywords: Air · Combustors · Design for testability · Fuels · Polybutadienes · Projectiles · Propulsion · Ramjet engines · Supersonic aerodynamics · Air-breathing propulsion · Delft University of Technology · Gun-launched projectile · High specific impulse · Hydroxy-terminated polybutadiene · Netherlands organization for applied scientific researches · Operational conditions · Sustained combustion · Combustion · Observation, Weapon & Protection Systems · EM - Energetic Materials
[Abstract]

20 Developments on HNF based high performance and green solid propellants
article 2001    
Author: Keizers, H.L.J. · Heijden, A.E.D.M. van der · Vliet, L.D. van · Welland-Veltmans, W.H.M. · Ciucci, A.
Keywords: Air pollution · Aircraft fuels · Cost effectiveness · Environmental engineering · Exhaust gases · Hydrochloric acid · Low temperature effects · Military aircraft · Morphology · Precipitation (chemical) · Recrystallization (metallurgy) · Rocket engines · Space flight · Space research · Spacecraft propulsion · Thermodynamic stability · Energetic binders systems · Space transportation · Solid propellants
[Abstract]

Search results also available in MS Excel format.

Showing 1 to 20 of 31 found. Next | Sort by date