AIAA Propulsion and Energy 2019 Forum 2019
DOI: 10.2514/6.2019-4392
|View full text |Cite
|
Sign up to set email alerts
|

Design and Additive Manufacturing Considerations for Liquid Rocket Engine Development

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
2
0

Year Published

2021
2021
2024
2024

Publication Types

Select...
4

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
(2 citation statements)
references
References 8 publications
0
2
0
Order By: Relevance
“…processes and several materials that can be used for this purpose, so that further implementations especially in CubeSats and other microsatellites and smaller satellites can be expected in the near future. Besides these technologies typically used in satellites, it is also possible to use different alloys for liquid rocket channel-wall nozzles [78,79] and other liquid rocket engine component applications [80,81], as well as to prepare composite propellant grains for solid rockets [82,83]. Another aspect, the reduction of manufacturing costs, was in the focus of a recent study of Hoffman and Grubisic who combined selective laser melting with off-the-shelf components to build a 20 cm-diameter microwave discharge ion thruster [72].…”
Section: Thrustersmentioning
confidence: 99%
See 1 more Smart Citation
“…processes and several materials that can be used for this purpose, so that further implementations especially in CubeSats and other microsatellites and smaller satellites can be expected in the near future. Besides these technologies typically used in satellites, it is also possible to use different alloys for liquid rocket channel-wall nozzles [78,79] and other liquid rocket engine component applications [80,81], as well as to prepare composite propellant grains for solid rockets [82,83]. Another aspect, the reduction of manufacturing costs, was in the focus of a recent study of Hoffman and Grubisic who combined selective laser melting with off-the-shelf components to build a 20 cm-diameter microwave discharge ion thruster [72].…”
Section: Thrustersmentioning
confidence: 99%
“…Besides these technologies typically used in satellites, it is also possible to use different alloys for liquid rocket channel-wall nozzles [78,79] and other liquid rocket engine component applications [80,81], as well as to prepare composite propellant grains for solid rockets [82,83].…”
Section: Thrustersmentioning
confidence: 99%