A Miniaturized, Green, End-Burning, and Sandwich Hybrid Propulsion System-Reference-Cited by-同舟云学术

A Miniaturized, Green, End-Burning, and Sandwich Hybrid Propulsion System

Published:2022-09 Issue:5 Volume:38 Page:701-713
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Smith Tyson K.¹,Lewis Zachary¹,Olsen Kurt¹,Bulcher Marc A.¹,Whitmore Stephen A.²^ORCID

Affiliation:

1. Space Dynamics Laboratory, North Logan, Utah 84341

2. Utah State University, Logan, Utah 84322-4130

Funder

Space Dynamics Laboratory

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B38623

Reference17 articles.

1. YostB.WestonS.DonoA.NguyenA.WickizerB.TrianoC.PiresC.MauroD.CannonH.StuplJ.HinesJ.MurbachM.CastleP.SubbaramanR.Ntone SikeR.ChristaS.WuS.StevensonT.SodermanT.BenavidesG.KamhawiH.HartwigJ.ElchertJ.ShastryR.SchneiderS.LiuT.FabanichW.MarshallW.JustisB.BanksB.WilcoxD.HudeckJ.SantosL.SheltonM.SchaireS.AltuncS.BundickS.WongY.CavenderD.BalintG.SchunkG.PolzinK.MauroS.GrahamL.HigginbothamS.ThomsenL.BuehrleR. D.HalesS.FonderS.ChandlerS.SkulskyE. D.StuartJ.ZiemerJ.KahnP.WilsonR.WoolleyR.LichtenS.ElyT.ReavesA.ArenaA.HsuA.BraunB.BradyB.O’QuinnC.VenturiniC.HinkleyD.BecklundD.CratesG.SkinnerM.MusaniR.UnverzagtR.SpektorR.KanterM.GoldbergerS.CurtissT.PaigeT.TsubotaT.PrerostJ.BulcherM.FeltM.TophamS.SmithT. K.LewisZ. “Small Spacecraft Technology State of the Art,” NASA Ames Research Center, Small Spacecraft Systems Virtual Inst., Oct. 2020, https://www.nasa.gov/smallsat-institute/sst-soa-2020.

2. Liquid-Fed Pulsed Plasma Thruster with Low-Energy Surface Flashover Igniter for Propelling Nanosatellites

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Satellite Cluster Flight Using Guidance Trajectory and Model Predictive Control;The Journal of the Astronautical Sciences;2024-03-07

2. Numerical Research on Mixing Combustion Characteristic of Vortex Flow Pancake Hybrid Rocket Motor;2024

3. Model predictive control switching strategy for safe small satellite cluster formation flight;Aerospace Systems;2023-07-26

4. Ignition processes and characteristics of charring conductive polymers with a cavity geometry in precombustion chamber for applications in micro/nano satellite hybrid rocket motors;Defence Technology;2023-05