• Produktbild: Space Engineering
  • Produktbild: Space Engineering
Band 15

Space Engineering Proceedings of the Second International Conference on Space Engineering

Fr. 72.90

inkl. gesetzl. MwSt., Versandkostenfrei


Beschreibung

Produktdetails

Einband

Taschenbuch

Erscheinungsdatum

06.03.2012

Herausgeber

G.A. Partel

Verlag

Springer Netherland

Seitenzahl

737

Maße (L/B/H)

24.4/17/4 cm

Gewicht

1260 g

Auflage

1970

Sprache

Englisch

ISBN

978-94-011-7553-1

Beschreibung

Produktdetails

Einband

Taschenbuch

Erscheinungsdatum

06.03.2012

Herausgeber

G.A. Partel

Verlag

Springer Netherland

Seitenzahl

737

Maße (L/B/H)

24.4/17/4 cm

Gewicht

1260 g

Auflage

1970

Sprache

Englisch

ISBN

978-94-011-7553-1

Herstelleradresse

Springer-Verlag KG
Sachsenplatz 4-6
1201 Wien
AT

Email: GPSR Kontakt

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  • Produktbild: Space Engineering
  • Produktbild: Space Engineering
  • Opening Ceremony.- Address.- I/Structures and Materials.- Vibrations of Thin Elastic Plates Subject to Random Driving Forces.- Designing Cost-Effective Pressure Vessels Based on Fracture Mechanics.- Investigation of Low ?s/?-Coatings in a Simulated Space Environment.- II/ Guidance And Control Systems.- Contrôle automatique des chaînes de télémesures.- Some Problems of Controlling Spaceships.- Numerical Procedures for the Attitude and Orbital Maneuvers Computation of a Spin-Stabilised Satellite.- A Roll and Pitch Attitude Control Scheme for a Synchronous, Flywheel Stabilized, Communication Satellite.- Autopilot Compatibility of the Digital Inertial Guidance System Used in the Eldo ‘Europa’ Launch Vehicle.- Development of the ‘Europa I’ First Stage attitude Control System to the ‘Europa II’ Requirements.- III/Propellants and Combustion, I.- Decomposition and Ignition of Ammonium Perchlorate in the Presence of SnO2-Cr2O3 Catalysts.- Advanced Chemical Rocket Propellants: On the Way from Theory to Hardware.- Advanced Fuels and Oxidizers.- Effect of Additives on the Combustion of Hydrazine/Nitrogen Tetroxide.- Effects of Propellant Injection on Resonant Combustion.- Analytical and Experimental Investigations of Aerothermochemical Processes in Liquid Propellant Rocket Motors.- IV/Propellants And Combustion, II.- Investigations on Propellant Vaporization and Gas Mixture Formation in a Liquid Rocket Motor Using Nonhypergolic Propellants.- Physical and Chemical Kinetics of Al and ? Flames (An Extended Abstract).- Investigation of Boron Combustion for Its Application in Air Augmented Rockets.- Propellant Expulsion Techniques.- Investigation of an Injector Concept for Throttleable High-Energy Rocket Engines.- V/Propulsion, I.- Determination of the Position of the Supersonic Flow Closing Shock Wave in the Channels of an Air-Breathing Jet Engine.- Reduction in Cost of the First Stage, ‘Recoverable’ First Stages, and First Stages ‘to Be Thrown Away’.- Low Cost Launch- and Re-Entry Vehicles - a Requirement for Future Space Flight.- Comparison of a Booster-Ram Rocket Combination with a Two-Stage Rocket for An Acceleration Mission.- Hybrid Motors in Sounding Rockets - Technical and Economical Advantages.- Evolution of Reaction Control Engines for U.S. Manned Spacecraft.- VI/Propulsion, II.- The Morphological Continuum in Solid Propellant Grain Design.- Une famille de propulseurs Bi-ergols à poussées comprises entre 40 et 1 kp. Technologie et possibilités d’application pour le Satellite ‘Symphonie’.- Design of the Apollo Service Module Rocket Engine for Manned Operation.- Some Problems of the Dynamics of a Space Vehicle with Tanks Partially Filled with Liquid.- VII/Auxiliary Power Systems.- Compact ZrH Reactor Development Status and Reactor Thermoelectric Space Power Systems.- Batteries d’accumulateurs pour alimentation en énergie de satellites.- Batteries d’accumulateurs souples nickel-cadmium pour alimentation de ballons météorologiques.- Low-Power Nuclear Energy Conversion for Long-Duration Space Missions. Comparison between Rankine and Brayton Cycles: Dynamic and MHD Power Conversion.- VIII/Testing, Support and Accessories, I.- Investigation of the Vibration Modes of a Three Degrees of Freedom Ground Testing Apparatus for the Attitude-Control System of Satellites.- Satellites and Heat-Shields Test Facilities at FIAT Aerospace Laboratory.- Jettisoning Test Equipment at FIAT Aerospace Laboratory.- A Comparison of Satellite Drag Measurement Techniques.- Satellite Gravitational Stabilization Systems with Maximum Damping Rate.- An Analysis and Simulation of Mars Landing.- The Deep Space Network. An Instrument for Radio Navigation for the Mariner Mission to Mars, 1969.- Optimal Value for the Antenna Spacing of a Three Antenna Interferometer.- IX/Testing, Support and Accessories, II.- Space Programme in India.- The Churchill Research Range and Canada’s Space Research Program.- Design and Dynamic Characteristics Investigation of a High Performance Spherical Bearing.- A Polyvalent Data Acquisition System for Ground Space Tests at FIAT Aerospace Laboratory.- Méthodes et moyens d’essais relatifs au développement des propulseurs.- New Capacitive Pressure Transducer for Aerospatial Use.- X/Speeches Delivered at the Banquet.- Speech by General B. A. Schriever: Manned Space Stations (Gateway to Our Future in Space).- Speech by Academician B. N. Petrov.