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 was patented by McDonnell Douglas (now part of Boeing).[1]
It is extremely light and stiff.[2] 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.
Top view of isogrid panelCross-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. 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.[5][6] Since the equilateral triangle pattern has isotropic strength characteristics (no preferential direction), it was named isogrid.[5]
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]
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.
^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
^US patent 4012549, Paul Slysh, "High strength composite structure", published Oct 10, 1974, issued Mar 15, 1977
^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. ISSN0263-8223.
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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.
^Meyer, R. R; Harwood, O. P. (Oct 1, 1973) [1973]. Isogrid design handbook. Marshall Space Flight Center. 19730000395.
^Slysh, Paul. "The Isogrid". Archived from the original on March 24, 2012. Retrieved May 27, 2011.
^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)
