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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 (or face sheet) with triangular integral stiffening ribs (often called stringers). It is extremely light and stiff.[1] Compared to other materials, it is expensive to manufacture, and so it is restricted to spaceflight applications and some particularly critical parts of more general aerospace use.

Theory and design[edit]

Top view of isogrid panel
Cross-section of isogrid flange stiffener[2]

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.[3]

The triangular pattern is very efficient because it retains rigidity while saving material and therefore weight. 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.

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.[4] Since the equilateral triangle pattern has isotropic strength characteristics (no preferential direction), it was named isogrid.[citation needed]


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 0.040 in. (1.0 millimeter) might require chemical milling processes.[5]

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.[6] This can give extremely high strength-weight ratios.[7]


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.

Some spacecraft and launch vehicles which use isogrid structures include:


  2. ^ US patent 4012549, Paul Slysh, "High strength composite structure", published Oct 10, 1974, issued Mar 15, 1977 
  3. ^ 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.
  4. ^ a b c Meyer, R. R; Harwood, O. P. (Oct 1, 1973) [1973]. Isogrid design handbook. Marshall Space Flight Center. 19730000395. Archived from the original (PDF) on Sep 30, 2010.
  5. ^ Slysh, Paul. "The Isogrid". Retrieved May 27, 2011.
  6. ^ 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. Elsevier. 33 (2): 155–161. doi:10.1016/S1359-835X(01)00113-0. Retrieved 26 May 2012.
  7. ^ 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.
  8. ^ Knighton, D. J. (Sep 1, 1972) [1972], Delta launch vehicle isogrid structure NASTRAN analysis, Goddard Space Flight Center, hdl:2060/19720025227, archived from the original on Jun 11, 2007
  9. ^ "Atlas V 500 series" (PDF). United Launch Alliance. Retrieved 2016-06-06.
  10. ^ Young, Anthony (23 June 2014). "Boeing displays CST-100 progress at Kennedy Space Center". The Space Review. SpaceNews. Retrieved 25 October 2017.
  11. ^ Wagner, W. A. (May 1, 1974) [1974], Liquid rocket metal tanks and tank components (PDF), NASA Lewis Research Center, pp. 55–58, hdl:2060/19750004950, archived from the original on Nov 22, 1995

External links[edit]