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[[File:Orion-Delta_IV_adapter_isogrid.jpg|thumb|right|Isogrid on the interior of the adapter connecting the Orion spacecraft to the Delta IV rocket for [[Exploration Flight Test 1]] ]]
{{morefootnotes|date=December 2010}}

An '''isogrid''' is a plate (or face sheet) with triangular integral stiffening ribs (often called stringers). The stiffeners of an isogrid are generally machined from a single sheet of material with a milling machine, though below 0.004 in. thickness chemical milling processes must be used.<ref name="theisogrid">{{cite web
'''Isogrid''' is a type of partially hollowed-out structure formed usually from a single metal plate with integral triangular stiffening [[stringer (aircraft)|stringer]]s. It was patented by [[McDonnell Douglas]] (now part of [[Boeing]]). {{Year needed|date=September 2024}}<ref>{{cite conference
| url = http://www.isogrid-sst.com/machine%20design.htm
|url=https://www.iccm-central.org/Proceedings/ICCM12proceedings/site/papers/pap357.pdf
| title = The Isogrid
|title= GRID STIFFENED STRUCTURES: A SURVEY OF FABRICATION, ANALYSIS AND DESIGN METHODS
| first = Paul
|last1= Huybrechts |first1= Steven M.
| last = Slysh
|last2= Hahn |first2= Steven E.
| accessdate = May 27, 2011
|last3= Meink |first3= Troy E.
}}</ref> The triangular pattern is very efficient because triangular trusses are very efficient structures. The term isogrid is used because the structure acts like an [[isotropic]] material, with equal properties measured in any direction, and grid, referring to the sheet and stiffeners structure.
|date= July 5–9, 1999
[[File:Isogrid_topview.png|thumb|Border|right|baseline||link=|alt=|Topview of Isogrid Panel]]
|location= Paris, France
Metal isogrids (often aluminum), are constructed by milling material from one face of a sheet.
|conference= Proceedings of the 1999 International Conference on Composite Materials
Composite isogrids are rib-skin{{clarify|date=December 2010}} configurations formed by various manual or automated processes, and can give extremely high strength-weight ratios.<ref name="afrl_ags">{{Cite conference
|access-date=Jan 10, 2020
| last = Wegner
|quote= The McDonnell-Douglas Corporation (now part of The Boeing Company) holds the patent rights for development of the first aluminum isogrid}}
| first = Peter M.
</ref>
| last2 = Higgins
Isogrids are extremely light and stiff.<ref>{{Cite thesis |type=PhD
| first2 = John E.
|last=Black |first=Jonathan T. |date=2006
| last3 = VanWest
|url=https://uknowledge.uky.edu/gradschool_diss/390/
| first3 = Barry P.
<!-- https://uknowledge.uky.edu/cgi/viewcontent.cgi?article=1393&context=gradschool_diss -->
| title = Application of Advanced Grid-Stiffened Structures Technology to the Minotaur Payload Fairing
|title=NEW ULTRA-LIGHTWEIGHT STIFF PANELS FOR SPACE APERTURES
| booktitle = 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
|publisher=University of Kentucky Doctoral Dissertations |access-date=Jan 10, 2020}}</ref> Compared to other materials, it is expensive to manufacture, and so it is restricted to [[spaceflight]] applications and some [[aerospace]] use. {{Citation needed|date=September 2024}}
| place = Denver, CO

| year = 2002
== Theory and design ==
| url = http://handle.dtic.mil/100.2/ADA510804}}</ref> Traditionally, the equilateral triangle pattern was used because it was amenable to simplified analysis.<ref name="isodesign_handbook">{{Citation
[[File:Isogrid topview.png|thumb|baseline|alt=|Top view of isogrid panel]]
| last = Meyer
[[File:Isogrid flange.png|thumb|baseline|alt=|Cross-section of isogrid flange stiffener<ref name="composite_iso">{{cite patent
| first = R. R
| last2 = Harwood
| first2 = O. P.
| last3 =
| first3 =
| title = Isogrid design handbook
| publisher = Marshall Space Flight Center
| date = Oct 1, 1973
| origyear = 1973
| year = 1973
| month = October
| language = English
| url = http://femci.gsfc.nasa.gov/Isogrid/NASA-CR-124075_Isogrid_Design.pdf
| archiveurl = http://ntrs.nasa.gov/search.jsp?R=19730000395&qs=Ns%3DNASA-Center|0%26N%3D4294753258
| archivedate = Sep 30, 2010
| id = 19730000395 }}</ref> Since the equilateral triangle pattern has isotropic strength characteristics (no preferntial direction), it was named <b>iso</b>grid. The traditional equilateral pattern can be abandoned in favor of stiffener patterns optimized to specified loading situations; these structures are referred to as composite grid structures or advanced grid stiffened (AGS) structures.{{citation needed|date=December 2010}}
[[File:Isogrid_flange.png|thumb|Border|right|baseline|link=|alt=|Cross-section of Isogrid Flange Stiffner<ref name="composite_iso">{{ cite patent
| country = US
| country = US
| number = 4012549
| number = 4012549
Line 46: Line 30:
| gdate = Mar 15, 1977
| gdate = Mar 15, 1977
| fdate = Oct 10, 1974
| fdate = Oct 10, 1974
| pridate =
| inventor = Paul Slysh
| inventor = Paul Slysh
| invent1 =
| invent2 =
| assign1 =
| assign2 =
| class =
}}</ref>
}}</ref>
]]
]]
Isogrid structures are related to [[sandwich-structured composite]] panels; both can be modeled using [[sandwich theory]], which describes structures with separated, stiff face sheets and a lighter interconnecting layer. Isogrids are manufactured from single sheets of material and with large-scale triangular openings, and an open pattern to the [[flange]]s, compared to closed sheets and foam or honeycomb structures for the sandwich-composite structures.

Isogrid structures are constituted by a thin skin reinforced with a lattice structure. Such structures are adopted in the aeronautical industry since they present both structural resistance and lightness.<ref>{{Cite journal|date=2016-05-20|title=Design and manufacturing of an isogrid structure in composite material: Numerical and experimental results|journal=Composite Structures|language=en|volume=143|pages=189–201|doi=10.1016/j.compstruct.2016.02.043|issn=0263-8223|last1=Sorrentino|first1=L.|last2=Marchetti|first2=M.|last3=Bellini|first3=C.|last4=Delfini|first4=A.|last5=Albano|first5=M.}}</ref>

The triangular pattern is very efficient because it retains rigidity while saving material and therefore weight. {{Citation needed|date=September 2024}} The term isogrid is used because the structure acts like an [[isotropic]] material, with equal properties measured in any direction, and grid, referring to the sheet and stiffeners structure. {{Citation needed|date=September 2024}}

{{anchor|Orthogrid}}A similar variant is the '''orthogrid''' (sometimes called a [[waffle]] grid), which uses [[rectangular tiling|rectangular]] rather than triangular openings. This is not isotropic (has different properties from different angles), but matches many [[use case]]s well and is easier to manufacture.

Traditionally, the [[triangular tiling|equilateral triangle pattern]] was used because it was amenable to simplified analysis.<ref name="isodesign_handbook">
{{cite tech report
|url=https://femci.gsfc.nasa.gov/isogrid/NASA-CR-124075_Isogrid_Design.pdf
|title=Isogrid Design Handbook
|author=McDonnell Douglas Astronautics Company
|date=February 1973
|publisher=NASA
|number=NASA CR-124075
|access-date=Jan 10, 2020
|page=1.0.002 (12/252)}}</ref>
<ref>{{cite book
|last1 = Meyer | first1 = R. R
|last2 = Harwood | first2 = O. P.
|title = Isogrid design handbook
|publisher = Marshall Space Flight Center
|date = Oct 1, 1973
|orig-year = 1973
|url=https://ntrs.nasa.gov/search.jsp?R=19730000395&qs=Ns%3DNASA-Center%7c0%26N%3D4294753258
|id=19730000395
}}</ref> Since the equilateral triangle pattern has isotropic strength characteristics (no preferential direction), it was named isogrid.<ref name="isodesign_handbook" />

== Manufacturing ==
The stiffeners of an isogrid are generally machined from one face of a single sheet of material such as [[Aluminium|aluminum]] with a [[Numerical control|CNC]] [[Milling (machining)|milling machine]]. A thickness less than {{convert|.04|in|mm}} might require [[chemical milling]] processes.<ref name="theisogrid">{{cite web
| url = http://www.isogrid-sst.com/machine%20design.htm
| archive-url=https://web.archive.org/web/20120324153516/http://www.isogrid-sst.com/machine%20design.htm
| archive-date= March 24, 2012
| url-status = live
| title = The Isogrid
| first = Paul | last = Slysh
| access-date = May 27, 2011
}}</ref>

A major push has been made toward [[3D printing|additive manufacturing]] techniques due to a decrease in overall material and production costs and high efficiency and accuracy while providing control over parameters like porosity. Also, the ease of prototype manufacturing for testing purposes has made a huge contribution.<ref>{{Cite web|last=Tripathi, Kukreja, Madan|title=Evolution in Manufacturing of Grid Stiffened Structures through CAM and Additive Techniques|url=https://www.researchgate.net/publication/351065515|website=Research Gate}}</ref>

Composite isogrids are rib-skin configurations, where at least a part of the rib is a different material from the skin, the composite assembled by various manual or automated processes.<ref name="gridstiffened_manufacturing">{{cite journal
| last = Huybrechts
| first = Steven
|author2=Troy E. Meink |author3=Peter M. Wegner
|author4=Jeff M. Ganley
| title = Manufacturing theory for advanced grid stiffened structures
| journal = Composites Part A: Applied Science and Manufacturing
| volume = 33
| issue = 2
| pages = 155–161
| publisher = Elsevier
| year = 2002
| url = http://oai.dtic.mil/oai/oai?verb=getRecord&metadataPrefix=html&identifier=ADA430878
| archive-url = https://web.archive.org/web/20160304055254/http://oai.dtic.mil/oai/oai?verb=getRecord&metadataPrefix=html&identifier=ADA430878
| url-status = dead
| archive-date = March 4, 2016
| access-date = 26 May 2012| doi = 10.1016/S1359-835X(01)00113-0
}}</ref>
This can give extremely high strength-weight ratios.<ref name="afrl_ags">{{Cite conference
| last1 = Wegner | first1 = Peter M.
| last2 = Higgins | first2 = John E.
| last3 = VanWest | first3 = Barry P.
| title = Application of Advanced Grid-Stiffened Structures Technology to the Minotaur Payload Fairing
| book-title = 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
| place = Denver, CO
| year = 2002
| url = http://handle.dtic.mil/100.2/ADA510804
| archive-url = https://web.archive.org/web/20120527163248/http://handle.dtic.mil/100.2/ADA510804
| url-status = dead
| archive-date = May 27, 2012
}}</ref>

== Uses ==
[[File:CST-100 pressure vessel.jpg|thumb|right|Isogrids on the [[CST-100]] pressure vessel]]
Isogrid panels form self-stiffened structures where low weight, stiffness, strength and damage tolerance are important, such as in aircraft or space vehicles.
Isogrid panels form self-stiffened structures where low weight, stiffness, strength and damage tolerance are important, such as in aircraft or space vehicles.
Aerospace isogrid structures include payload shrouds, and boosters which must support the full weight of upper stages and payloads under high G loads.
Aerospace isogrid structures include payload shrouds and boosters, which must support the full weight of upper stages and payloads under high G loads. Their open configuration with a single, sealed sheet facing the outside makes them especially useful for propellant tanks for rockets, where sealing the propellant in, but allowing it to drain in use or maintenance are necessary features. {{Citation needed|date=September 2024}}


== Examples ==
Some spacecraft and launch vehicles which use isogrid structures include:
Some spacecraft and launch vehicles which use isogrid structures include:
* [[Delta rocket|Delta]] families <ref name="isodesign_handbook"></ref><ref name="delta_iso_nastran">{{Citation
* [[Delta rocket|Delta]] families<ref name="isodesign_handbook" /><ref name="delta_iso_nastran">{{Citation
|last = Knighton
| last = Knighton, D. J.
| first = D.J.
|first = D. J.
| title = Delta launch vehicle isogrid structure NASTRAN analysis
|title = Delta launch vehicle isogrid structure NASTRAN analysis
|journal = Nastran: Users' Experiences
| publisher = Goddard Space Flight Center
|publisher = Goddard Space Flight Center
| date = Sep 1, 1972
| origyear = 1972
|date = Sep 1, 1972
| year = 1972
|orig-year = 1972
|hdl = 2060/19720025227
| month = September
|url = https://ntrs.nasa.gov/search.jsp?R=19720025227
| language = English
| url = http://hdl.handle.net/2060/19720025227
|archive-url = https://web.archive.org/web/20210129191829/https://ntrs.nasa.gov/search.jsp?R=19720025227
|archive-date = January 29, 2021
| archiveurl = http://ntrs.nasa.gov/search.jsp?R=19720025227&qs=Ns%3DLoaded-Date|1%26N%3D4294759313
|access-date = July 7, 2017
| archivedate = Jun 11, 2007
|url-status = bot: unknown
| id = 19720025227 }}</ref>
}}</ref>
* [[Atlas V]] rocket {{citation needed|date=May 2011}}
* [[Atlas (rocket family)|Atlas]] families<ref>{{Cite web|url=http://www.ulalaunch.com/uploads/docs/Atlas500_Cutaway.pdf|title=Atlas V 500 series|publisher=United Launch Alliance|access-date=2016-06-06|archive-url=https://web.archive.org/web/20160409203927/http://www.ulalaunch.com/uploads/docs/Atlas500_Cutaway.pdf|archive-date=2016-04-09|url-status=dead}}</ref>
* [[Skylab]] spacestation Orbital Workshop module <ref name="isodesign_handbook"></ref>
* [[Skylab]] spacestation Orbital Workshop module<ref name="isodesign_handbook" />
* [[CST-100]] crew capsule {{citation needed|date=May 2011}}
* [[Space Launch System#Core stage|SLS Core Stage]]<ref>{{cite web
* [[Dragon_(spacecraft)|Dragon]] crew capsule {{citation needed|date=May 2011}}
|url=https://www.spacelaunchreport.com/sls7.html
* [[Multi_Purpose_Crew_Vehicle|MPCV]] formerly [[Orion_(spacecraft)|Orion]] crew capsule {{citation needed|date=May 2011}}
|archive-url=https://web.archive.org/web/20140404120940/http://spacelaunchreport.com/sls7.html
|url-status=usurped
|archive-date=April 4, 2014
|title=Progress on NASA's Space Launch System and Orion
|last= Kyle
|first= Ed
|date=Jan 26, 2014
|website=Space Launch Report
|access-date=Jan 10, 2020
|quote=Boeing's SLS core will use AL-2219 Aluminum machined with isogrids}}
</ref>
* [[CST-100 Starliner]]<ref>{{cite news|last1=Young|first1=Anthony|title=Boeing displays CST-100 progress at Kennedy Space Center|url=http://www.thespacereview.com/article/2538/1|access-date=25 October 2017|work=The Space Review|publisher=[[SpaceNews]]|date=23 June 2014}}</ref>
* [[SpaceX|Spacex]] [[SpaceX Dragon 2|Crew Dragon]]<ref>{{Cite web |last=Editor |first=SpaceRef |date=2010-10-05 |title=SpaceX Update: COTS Demonstration Flight 1 (with photos) |url=https://spaceref.com/status-report/spacex-update-cots-demonstration-flight-1-with-photos/ |access-date=2022-11-03 |website=SpaceRef |language=en-US}}</ref>
=== Orthogrid ===
Orthogrid (also known as waffle grid) is similar to isogrid, but with a square pattern; examples include:
* [[Saturn (rocket family)|Saturn]] rocket tanks, due to the lower cost and ease of manufacture<ref name="liquid_rocket_tanks" >{{Citation
| last = Wagner
| first = W. A.
| title = Liquid rocket metal tanks and tank components
| publisher = NASA Lewis Research Center
| date = May 1, 1974
| orig-year = 1974
| hdl = 2060/19750004950
| pages = 55–58
| url = https://ntrs.nasa.gov/search.jsp?R=19750004950
| archive-url = https://web.archive.org/web/20210130173055/https://ntrs.nasa.gov/search.jsp?R=19750004950
| archive-date = January 30, 2021
| access-date = November 26, 2019
| url-status = bot: unknown
}}</ref>
* [[Vulcan (rocket)|Vulcan]] rocket<ref>{{cite tweet |last=Bruno |first=Tory |user=torybruno |number=855031915270635522 |date=Apr 20, 2017 |title=Orthogrid trial panel for Vulcan Rocket propellant tank. (Bigger than it looks...) |link=https://twitter.com/torybruno/status/855031915270635522 |access-date=Jan 10, 2020}}</ref>
* [[New Glenn]] rocket tanks
* [[Space Launch System core stage]] tanks


{{Clear}}
The [[Space Shuttle]] [[Space Shuttle External Tank#Lightweight Tank|lightweight and superlightweight]] external tanks use an integrally machined stringer system which is not a true isogrid, though it is somewhat similar. Since the structure is arranged at right angles it is considered an "orthogrid" rather than an isogrid with triangular stiffeners of an isogrid.{{citation needed|date=December 2010}}


==See also==
Isogrids are beginning to be used in consumer products where extremely light weight, strength, and stiffness are important, like tennis rackets.{{citation needed|date=December 2010}}
* [[Honeycomb structure]]
* [[Hollow structural section]]
* [[Space frame]]
* [[Speed holes]]
* [[Truss]]
* [[Waffle slab]], concrete structure similar to orthogrid
{{clear}}


==References==
==References==
Line 89: Line 184:
* [http://femci.gsfc.nasa.gov/Isogrid/ Isogrid Plate Modeling, Dr Wiliam Case, 1997]
* [http://femci.gsfc.nasa.gov/Isogrid/ Isogrid Plate Modeling, Dr Wiliam Case, 1997]
* [http://femci.gsfc.nasa.gov/Isogrid/NASA-CR-124075_Isogrid_Design.pdf Isogrid Design Handbook, NASA CR-124075, McDonnell Douglas, 1973]
* [http://femci.gsfc.nasa.gov/Isogrid/NASA-CR-124075_Isogrid_Design.pdf Isogrid Design Handbook, NASA CR-124075, McDonnell Douglas, 1973]
* [http://composite.about.com/library/weekly/aa980525.htm Advanced Grid Stiffened Composite Structures]
* [http://composite.about.com/library/weekly/aa980525.htm Advanced Grid Stiffened Composite Structures] {{Webarchive|url=https://web.archive.org/web/20060422101203/http://composite.about.com/library/weekly/aa980525.htm |date=2006-04-22 }}
* [http://Isogrid-SST.com/referenc.htm Isogrid - Shell Structures Tools, 1990]
* [http://Isogrid-SST.com/referenc.htm Isogrid - Shell Structures Tools, 1990] {{Webarchive|url=https://web.archive.org/web/20110713063212/http://isogrid-sst.com/referenc.htm |date=2011-07-13 }}
* [http://www.sheldrake.net/quarter_isogrid/ Quarter Isogrid used in Surfboard Construction]


{{commonscat|Isogrid}}
[[Category:Components]]
{{Authority control}}


[[Category:Components]]
[[ja:アイソグリッド構造]]
[[Category:Aerospace materials]]

Latest revision as of 19:08, 25 September 2024

Isogrid on the interior of the adapter connecting the Orion spacecraft to the Delta IV rocket for Exploration Flight Test 1

Isogrid is a type of partially hollowed-out structure formed usually from a single metal plate with integral triangular stiffening stringers. It was patented by McDonnell Douglas (now part of Boeing). [year needed][1] Isogrids are extremely light and stiff.[2] Compared to other materials, it is expensive to manufacture, and so it is restricted to spaceflight applications and some aerospace use. [citation needed]

Theory and design

[edit]
Top view of isogrid panel
Cross-section of isogrid flange stiffener[3]

Isogrid structures are related to sandwich-structured composite panels; both can be modeled using sandwich theory, which describes structures with separated, stiff face sheets and a lighter interconnecting layer. Isogrids are manufactured from single sheets of material and with large-scale triangular openings, and an open pattern to the flanges, compared to closed sheets and foam or honeycomb structures for the sandwich-composite structures.

Isogrid structures are constituted by a thin skin reinforced with a lattice structure. Such structures are adopted in the aeronautical industry since they present both structural resistance and lightness.[4]

The triangular pattern is very efficient because it retains rigidity while saving material and therefore weight. [citation needed] The term isogrid is used because the structure acts like an isotropic material, with equal properties measured in any direction, and grid, referring to the sheet and stiffeners structure. [citation needed]

A similar variant is the orthogrid (sometimes called a waffle grid), which uses rectangular rather than triangular openings. This is not isotropic (has different properties from different angles), but matches many use cases well and is easier to manufacture.

Traditionally, the equilateral triangle pattern was used because it was amenable to simplified analysis.[5] [6] Since the equilateral triangle pattern has isotropic strength characteristics (no preferential direction), it was named isogrid.[5]

Manufacturing

[edit]

The stiffeners of an isogrid are generally machined from one face of a single sheet of material such as aluminum with a CNC milling machine. A thickness less than .04 inches (1.0 mm) might require chemical milling processes.[7]

A major push has been made toward additive manufacturing techniques due to a decrease in overall material and production costs and high efficiency and accuracy while providing control over parameters like porosity. Also, the ease of prototype manufacturing for testing purposes has made a huge contribution.[8]

Composite isogrids are rib-skin configurations, where at least a part of the rib is a different material from the skin, the composite assembled by various manual or automated processes.[9] This can give extremely high strength-weight ratios.[10]

Uses

[edit]
Isogrids on the CST-100 pressure vessel

Isogrid panels form self-stiffened structures where low weight, stiffness, strength and damage tolerance are important, such as in aircraft or space vehicles. Aerospace isogrid structures include payload shrouds and boosters, which must support the full weight of upper stages and payloads under high G loads. Their open configuration with a single, sealed sheet facing the outside makes them especially useful for propellant tanks for rockets, where sealing the propellant in, but allowing it to drain in use or maintenance are necessary features. [citation needed]

Examples

[edit]

Some spacecraft and launch vehicles which use isogrid structures include:

Orthogrid

[edit]

Orthogrid (also known as waffle grid) is similar to isogrid, but with a square pattern; examples include:

See also

[edit]

References

[edit]
  1. ^ Huybrechts, Steven M.; Hahn, Steven E.; Meink, Troy E. (July 5–9, 1999). GRID STIFFENED STRUCTURES: A SURVEY OF FABRICATION, ANALYSIS AND DESIGN METHODS (PDF). Proceedings of the 1999 International Conference on Composite Materials. Paris, France. Retrieved Jan 10, 2020. The McDonnell-Douglas Corporation (now part of The Boeing Company) holds the patent rights for development of the first aluminum isogrid
  2. ^ Black, Jonathan T. (2006). NEW ULTRA-LIGHTWEIGHT STIFF PANELS FOR SPACE APERTURES (PhD). University of Kentucky Doctoral Dissertations. Retrieved Jan 10, 2020.
  3. ^ US patent 4012549, Paul Slysh, "High strength composite structure", published Oct 10, 1974, issued Mar 15, 1977 
  4. ^ Sorrentino, L.; Marchetti, M.; Bellini, C.; Delfini, A.; Albano, M. (2016-05-20). "Design and manufacturing of an isogrid structure in composite material: Numerical and experimental results". Composite Structures. 143: 189–201. doi:10.1016/j.compstruct.2016.02.043. ISSN 0263-8223.
  5. ^ a b c d McDonnell Douglas Astronautics Company (February 1973). Isogrid Design Handbook (PDF) (Technical report). NASA. p. 1.0.002 (12/252). NASA CR-124075. Retrieved Jan 10, 2020.
  6. ^ Meyer, R. R; Harwood, O. P. (Oct 1, 1973) [1973]. Isogrid design handbook. Marshall Space Flight Center. 19730000395.
  7. ^ Slysh, Paul. "The Isogrid". Archived from the original on March 24, 2012. Retrieved May 27, 2011.
  8. ^ Tripathi, Kukreja, Madan. "Evolution in Manufacturing of Grid Stiffened Structures through CAM and Additive Techniques". Research Gate.{{cite web}}: CS1 maint: multiple names: authors list (link)
  9. ^ Huybrechts, Steven; Troy E. Meink; Peter M. Wegner; Jeff M. Ganley (2002). "Manufacturing theory for advanced grid stiffened structures". Composites Part A: Applied Science and Manufacturing. 33 (2). Elsevier: 155–161. doi:10.1016/S1359-835X(01)00113-0. Archived from the original on March 4, 2016. Retrieved 26 May 2012.
  10. ^ Wegner, Peter M.; Higgins, John E.; VanWest, Barry P. (2002). "Application of Advanced Grid-Stiffened Structures Technology to the Minotaur Payload Fairing". 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Denver, CO. Archived from the original on May 27, 2012.
  11. ^ Knighton, D. J. (Sep 1, 1972) [1972], "Delta launch vehicle isogrid structure NASTRAN analysis", Nastran: Users' Experiences, Goddard Space Flight Center, hdl:2060/19720025227, archived from the original on January 29, 2021, retrieved July 7, 2017{{citation}}: CS1 maint: bot: original URL status unknown (link)
  12. ^ "Atlas V 500 series" (PDF). United Launch Alliance. Archived from the original (PDF) on 2016-04-09. Retrieved 2016-06-06.
  13. ^ Kyle, Ed (Jan 26, 2014). "Progress on NASA's Space Launch System and Orion". Space Launch Report. Archived from the original on April 4, 2014. Retrieved Jan 10, 2020. Boeing's SLS core will use AL-2219 Aluminum machined with isogrids{{cite web}}: CS1 maint: unfit URL (link)
  14. ^ Young, Anthony (23 June 2014). "Boeing displays CST-100 progress at Kennedy Space Center". The Space Review. SpaceNews. Retrieved 25 October 2017.
  15. ^ Editor, SpaceRef (2010-10-05). "SpaceX Update: COTS Demonstration Flight 1 (with photos)". SpaceRef. Retrieved 2022-11-03. {{cite web}}: |last= has generic name (help)
  16. ^ Wagner, W. A. (May 1, 1974) [1974], Liquid rocket metal tanks and tank components, NASA Lewis Research Center, pp. 55–58, hdl:2060/19750004950, archived from the original on January 30, 2021, retrieved November 26, 2019{{citation}}: CS1 maint: bot: original URL status unknown (link)
  17. ^ Bruno, Tory [@torybruno] (Apr 20, 2017). "Orthogrid trial panel for Vulcan Rocket propellant tank. (Bigger than it looks...)" (Tweet). Retrieved Jan 10, 2020 – via Twitter.
[edit]
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