rdf-syntax-grammar
mods:
  schema location: http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
  title info:
    title: Space micropropulsion for nanosatellites
    sub title: progress, challenges and future
  name:
    name part: Cheah, Kean How.
  name:
    name part: ScienceDirect (Online service)
  type of resource: text
  genre: Electronic books.
  origin info:
    place:
      place term: ne
    place:
      place term: Amsterdam
    publisher: Elsevier
    date issued: 2022
    issuance: monographic
  language:
    language term: eng
  physical description:
    form: remote
    extent: 1 online resource (330 pages)
  abstract: Space Micropropulsion for Nanosatellites: Progress, Challenges and Future features the latest developments and progress, the challenges faced by different researchers, and insights on future micropropulsion systems. Nanosatellites, in particular cubesats, are an effective test bed for new technologies in outer space. However, most of the nanosatellites have no propulsion system, which subsequently limits their maneuverability in space.
  table of contents: Front Cover -- Space Micropropulsion for Nanosatellites -- Space Micropropulsion for Nanosatellites Progress, Challenges and Future -- Copyright -- Contents -- Contributors -- 1 -- Introduction -- 1 -- Emerging of nanosatellites -- 1.1 Philosophy of micro- and nanosatellites -- 1.2 The birth of CubeSats -- 1.3 Launching of CubeSats -- 1.4 First CubeSats -- 1.5 CubeSats for scientific missions and commercialization -- 1.6 CubeSats beyond the Earth -- 1.7 The need of micropropulsion system -- References -- 2 -- Chemical micropropulsions -- 2 -- Cold gas microthruster
  table of contents: 2.1 Background and principles of operation -- 2.2 Nozzle theory -- 2.3 Selection of propellant -- 2.4 State of the art-system with flight heritage -- 2.4.1 SNAP-1 (SSTL) -- 2.4.2 MEPSI (The Aerospace Corporation) -- 2.4.3 CanX-2 and CanX-4/5 (UTIAS/SFL) -- 2.4.4 Delfi-n3xt (TNO, U. Twente, and TU Delft) -- 2.4.5 POPSAT-HIP1 (microspace) -- 2.4.6 PRISMA, TW-1A and GomX-4B (NanoSpace) -- 2.4.7 NanoACE and MarCO (VACCO) -- 2.4.8 BEVO-2 and ARMADILLO (University of Texas at Austin) -- 2.5 Challenges and future -- 2.5.1 Miniaturization of nozzle via MEMS approach
  table of contents: 2.5.2 Optimization of micronozzle design -- 2.5.2.1 Past developments -- 2.5.2.2 Current developments -- References -- 3 -- Solid-propellant microthruster -- 3.1 Introduction -- 3.2 Solid propellants -- 3.2.1 Fuel -- 3.2.2 Oxidizer -- 3.2.3 Other reactants -- 3.2.4 Propellants -- 3.3 Solid-propellant propulsion fundamentals -- 3.3.1 Thrust chamber pressure and stability -- 3.3.2 Combustion model -- 3.4 Design of solid-propellant thruster -- 3.5 Progress in solid-propellant microthruster -- 3.5.1 Non-MEMS microthruster -- 3.5.2 MEMS-based microthruster -- 3.6 Conclusion and future prospects
  table of contents: 4.3.3 From small satellites into nanosatellites -- 4.3.3.1 LituanicaSAT-2 -- 4.3.3.2 M6P -- 4.3.3.3 ELSA-1d -- 4.3.3.4 ArgoMoon and Lunar Flashlight -- 4.3.3.5 Pathfinder Technology Demonstration (PTD) -- 4.3.4 Under development -- 4.3.4.1 MR-140 hydrazine thrusters -- 4.3.4.2 MPS-120 hydrazine and MPS-130 green propellant thrusters -- 4.3.4.3 GR-1A and GR-M1 thrusters -- 4.3.4.4 Pinot-G -- 4.3.4.5 BGT-X1 and X5 -- 4.3.4.6 Green mono-propellant micropropulsion system -- 4.3.4.7 MPUC -- 4.3.4.8 PM200 -- 4.4 Challenges and future -- 4.4.1 Bipropellant micropropulsion system
  note: edited by Kean How Cheah.
  note: 4.4.2 Monopropellant micropropulsion system.
  note: References-4-Liquid propellant microthrusters-4.1 Historical background and principles of operation-4.1.1 Operating principles-4.2 Liquid propellants-4.2.1 Performance of propellant-4.2.2 From bipropellant to monopropellant-4.2.3 From macroscale to microscale-4.2.4 Emerging of energetic ionic liquids as green propellant-4.3 State-of-the-art liquid propellant microthruster-4.3.1 Hydrazine thrusters-4.3.2 EILs-based green propellant thrusters-4.3.2.1 1 N HPGP propulsion system-4.3.2.2 1 N green propellant reaction control system-4.3.2.3 1 N GR-1 thruster.
  subject:
    topic: Nanosatellites
    topic: Propulsion systems
  subject:
    topic: Microspacecraft
  subject:
    topic: Nanosatellites
    topic: Propulsion
  subject:
    topic: Petits véhicules spatiaux
  subject:
    topic: Microspacecraft
  subject:
    topic: Nanosatellites
    topic: Propulsion systems
  classification: TL795.4
  classification: 629.46
  related item:
    title info:
      title: Space Micropropulsion for Nanosatellites
    name:
      name part: Cheah, Kean How.
    origin info:
      publisher: San Diego : Elsevier, ©2022
  identifier: 9780128190388
  identifier: 0128190388
  identifier: 9780128190371
  identifier: 012819037X
  identifier: 9780128190388 Ingram Content Group
  identifier: http://proxy.library.tamu.edu/login
  record info:
    record content source: EBLCP
    record creation date: 220326
    record change date: 20260327171821.7
    record identifier: in00005769551
    language of cataloging:
      language term: eng