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Space micropropulsion for nanosatell...

Cheah, Kean How.

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Space micropropulsion for nanosatellites = progress, challenges and future /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Space micropropulsion for nanosatellites/ edited by Kean How Cheah.
Reminder of title:	progress, challenges and future /
other author:	Cheah, Kean How.
Published:	Amsterdam :Elsevier, : 2022.,
Description:	1 online resource (330 p.)
[NT 15003449]:	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
[NT 15003449]:	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 andCanX-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
[NT 15003449]:	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
[NT 15003449]:	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 propulsionsystem-4.3.2.2 1 N green propellant reaction control system-4.3.2.3 1 N GR-1 thruster.
[NT 15003449]:	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
[NT 15003449]:	4.4.2 Monopropellant micropropulsion system.
Subject:	Nanosatellites - Propulsion systems. -
Online resource:	https://www.sciencedirect.com/science/book/9780128190371
ISBN:	9780128190388

Space micropropulsion for nanosatellites = progress, challenges and future /
Space micropropulsion for nanosatellitesprogress, challenges and future /[electronic resource] :edited by Kean How Cheah. - Amsterdam :Elsevier,2022. - 1 online resource (330 p.)

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

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.

ISBN: 9780128190388Subjects--Topical Terms:

3794261
Nanosatellites
--Propulsion systems.Index Terms--Genre/Form:

542853
Electronic books.

LC Class. No.: TL795.4

Dewey Class. No.: 629.46

Space micropropulsion for nanosatellites = progress, challenges and future /
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505 0 $a 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
505 8 $a 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 andCanX-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
505 8 $a 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
505 8 $a 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 propulsionsystem-4.3.2.2 1 N green propellant reaction control system-4.3.2.3 1 N GR-1 thruster.
505 8 $a 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
505 8 $a 4.4.2 Monopropellant micropropulsion system.
520 $a 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.
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700 1 $a Cheah, Kean How. $3 3794260
776 0 8 $i Print version: $a Cheah, Kean How. $t Space Micropropulsion for Nanosatellites. $d San Diego : Elsevier, ©2022 $z 9780128190371
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