The engineering knowledge required to design a spacecraft is spread across dozens of specialist textbooks, standards documents, and conference proceedings — each excellent within its discipline, none connecting the whole.
This handbook closes that gap.
Twenty chapters develop every major spacecraft subsystem at working-engineer depth — governing equations derived, not just stated; numerical examples carried to computed results; and cross-references that trace every output to the inputs it feeds in every adjacent chapter. A single spacecraft — a 1,500 kg Earth observation satellite in Sun-synchronous orbit at 500 km — runs as the worked example throughout, so every formula lands on real numbers and every result is traceable across the full design.
Coverage includes:
Both heritage-qualified and commercial new space practice — reusable launch vehicles, rideshare, mega-constellation operations, software-defined ground infrastructure — are addressed throughout. ECSS and CCSDS standards provide the governing framework where they apply.
For engineers entering spacecraft programmes or transitioning into systems roles; graduate students seeking a comprehensive systems-level reference; and practitioners who need one structured resource that connects every discipline and every decision.
Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.
Vendeur : Grand Eagle Retail, Bensenville, IL, Etats-Unis
Paperback. Etat : new. Paperback. The engineering knowledge required to design a spacecraft is spread across dozens of specialist textbooks, standards documents, and conference proceedings - each excellent within its discipline, none connecting the whole.This handbook closes that gap.Twenty chapters develop every major spacecraft subsystem at working-engineer depth - governing equations derived, not just stated; numerical examples carried to computed results; and cross-references that trace every output to the inputs it feeds in every adjacent chapter. A single spacecraft - a 1,500 kg Earth observation satellite in Sun-synchronous orbit at 500 km - runs as the worked example throughout, so every formula lands on real numbers and every result is traceable across the full design.Coverage includes: Space environment: radiation dose, plasma charging, atomic oxygen flux, thermal cycling, and debris risk - and how each constrains every subsystem that followsOrbital mechanics and mission analysis: vis-viva equation, eclipse fraction, nodal regression, constellation designChemical and electric propulsion sizing: specific impulse trades, propellant mass computation, and the power-transfer time tradeoff for all-electric platformsElectrical power systems: solar array sizing and degradation, battery management, power conditioning architecture, eclipse and sunlit mode budgetsAttitude determination and control: disturbance torque analysis, sensor and actuator selection, linearised control lawsStructures: launch load cases, natural frequency requirements, material selection, ECSS-compliant design marginsThermal control: coating selection, MLI sizing, radiator area, heater allocation, eclipse-sunlit cyclingTelecommunications: link budget development, Friis transmission equation, noise temperature, uplink and downlink marginTelemetry, command, and on-board data handling; EMC and ECSS-compliant verification; AIV test sequencing and model philosophySmall satellite and CubeSat systems engineering at genuine design depth - subsystem selection under real mass, power, and volume constraintsModel-based systems engineering: SysML architecture modelling, interface control, requirement traceability, digital twin integrationBoth heritage-qualified and commercial new space practice - reusable launch vehicles, rideshare, mega-constellation operations, software-defined ground infrastructure - are addressed throughout. ECSS and CCSDS standards provide the governing framework where they apply.For engineers entering spacecraft programmes or transitioning into systems roles; graduate students seeking a comprehensive systems-level reference; and practitioners who need one structured resource that connects every discipline and every decision. This item is printed on demand. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. N° de réf. du vendeur 9798187821204
Quantité disponible : 1 disponible(s)
Vendeur : California Books, Miami, FL, Etats-Unis
Etat : New. Print on Demand. N° de réf. du vendeur I-9798187821204
Quantité disponible : Plus de 20 disponibles
Vendeur : PBShop.store US, Wood Dale, IL, Etats-Unis
PAP. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur L2-9798187821204
Quantité disponible : Plus de 20 disponibles
Vendeur : PBShop.store UK, Fairford, GLOS, Royaume-Uni
PAP. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur L2-9798187821204
Quantité disponible : Plus de 20 disponibles
Vendeur : CitiRetail, Stevenage, Royaume-Uni
Paperback. Etat : new. Paperback. The engineering knowledge required to design a spacecraft is spread across dozens of specialist textbooks, standards documents, and conference proceedings - each excellent within its discipline, none connecting the whole.This handbook closes that gap.Twenty chapters develop every major spacecraft subsystem at working-engineer depth - governing equations derived, not just stated; numerical examples carried to computed results; and cross-references that trace every output to the inputs it feeds in every adjacent chapter. A single spacecraft - a 1,500 kg Earth observation satellite in Sun-synchronous orbit at 500 km - runs as the worked example throughout, so every formula lands on real numbers and every result is traceable across the full design.Coverage includes: Space environment: radiation dose, plasma charging, atomic oxygen flux, thermal cycling, and debris risk - and how each constrains every subsystem that followsOrbital mechanics and mission analysis: vis-viva equation, eclipse fraction, nodal regression, constellation designChemical and electric propulsion sizing: specific impulse trades, propellant mass computation, and the power-transfer time tradeoff for all-electric platformsElectrical power systems: solar array sizing and degradation, battery management, power conditioning architecture, eclipse and sunlit mode budgetsAttitude determination and control: disturbance torque analysis, sensor and actuator selection, linearised control lawsStructures: launch load cases, natural frequency requirements, material selection, ECSS-compliant design marginsThermal control: coating selection, MLI sizing, radiator area, heater allocation, eclipse-sunlit cyclingTelecommunications: link budget development, Friis transmission equation, noise temperature, uplink and downlink marginTelemetry, command, and on-board data handling; EMC and ECSS-compliant verification; AIV test sequencing and model philosophySmall satellite and CubeSat systems engineering at genuine design depth - subsystem selection under real mass, power, and volume constraintsModel-based systems engineering: SysML architecture modelling, interface control, requirement traceability, digital twin integrationBoth heritage-qualified and commercial new space practice - reusable launch vehicles, rideshare, mega-constellation operations, software-defined ground infrastructure - are addressed throughout. ECSS and CCSDS standards provide the governing framework where they apply.For engineers entering spacecraft programmes or transitioning into systems roles; graduate students seeking a comprehensive systems-level reference; and practitioners who need one structured resource that connects every discipline and every decision. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. N° de réf. du vendeur 9798187821204
Quantité disponible : 1 disponible(s)
Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Taschenbuch. Etat : Neu. Neuware. N° de réf. du vendeur 9798187821204
Quantité disponible : 2 disponible(s)