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Core & Void Filling Materials for Aerospace Composites

GracoRoberts supplies core and void filling materials for aerospace composite manufacturing, structural bonding, and repair applications. These materials are used to fill gaps and cavities, join honeycomb core sections, and provide localized support around edges, inserts, and transitions within composite sandwich structures.

Our portfolio includes composite resin fillers such as epoxy syntactic foams and structural void filling compounds, along with core splice adhesive films and expanding syntactic films from leading manufacturers including 3M, Huntsman, Henkel, and Resin Formulators. Available in cartridges, kits, sheets, and rolls, these materials support a range of composite fabrication and processing requirements.

For related materials used in composite manufacturing, explore our prepreg materials and composite process materials.

Core & Void Filling Materials

GracoRoberts P/N: 
V01252
MFR PN: 
7010329568 ...
7010329568 | 7010365975 | 7010365976
Estimated lead time 66 business days
GracoRoberts P/N: 
V00553
MFR PN: 
7000046402 ...
7000046402 | 7000046403 | 7000058937 | 7000121246 | 7000121247 | 7010301042 | 7100020520
From $121.56
Estimated lead time 75 business days
GracoRoberts P/N: 
V00555
MFR PN: 
7010365979 ...
7010365979 | 7010399451 | 7100006478
From $180.27
Estimated lead time 65 business days
GracoRoberts P/N: 
151423-100
MFR PN: 
7010309768
$407.82
Estimated lead time 85 business days
Known to cause cancer
Known to cause cancer
Classed as hazardous for shipping
Classed as hazardous for shipping
GracoRoberts P/N: 
124456-100
MFR PN: 
7100190505
$149.28
Estimated lead time 60 business days
GracoRoberts P/N: 
V01637
MFR PN: 
7100176150 ...
7100176150 | 7100217626
From $308.34
Estimated lead time 67 business days
GracoRoberts P/N: 
V00066
MFR PN: 
7000046493 ...
7000046493 | 7100027071
From $380.00
Estimated lead time 65 business days
GracoRoberts P/N: 
V01137
MFR PN: 
7000133727 ...
7000133727 | 7000133728
From $181.29
Estimated lead time 80 business days
GracoRoberts P/N: 
V01200
MFR PN: 
7100283398 ...
7100283398 | 7100283399 | 7100283415 | 7100283423
From $575.44
In Stock
GracoRoberts P/N: 
V01590
MFR PN: 
7000080057 ...
7000080057 | 7000080058
From $2,665.35
Estimated lead time 60 business days
GracoRoberts P/N: 
V01610
MFR PN: 
7100001271 ...
7100001271 | 7100241180
From $3,416.01
In Stock
GracoRoberts P/N: 
157722-100
MFR PN: 
7100176746
$5,140.44
Estimated lead time 20 business days
Classed as hazardous for shipping
Classed as hazardous for shipping
GracoRoberts P/N: 
V00072
MFR PN: 
7000133726 ...
7000133726 | 7010304397 | 7100176352
From $154.31
Estimated lead time 46 business days
GracoRoberts P/N: 
V00304
MFR PN: 
1840308 ...
1840308 | 1909908 | 4587108 | 4587208 | 4750308
From $911.24
Estimated lead time 95 business days
GracoRoberts P/N: 
V00254
MFR PN: 
1479108 ...
1479108 | 1816808 | 1912208
From $664.91
Estimated lead time 95 business days
GracoRoberts P/N: 
101208-100
MFR PN: 
1771708
Only available to US customers
Only available to US customers
Known to cause cancer and reproductive harm
Known to cause cancer and reproductive harm
Classed as hazardous for shipping
Classed as hazardous for shipping
GracoRoberts P/N: 
154621-100
MFR PN: 
4942808
Only available to US customers
Only available to US customers
Known to cause cancer and reproductive harm
Known to cause cancer and reproductive harm
GracoRoberts P/N: 
101157-100
MFR PN: 
1819508
$715.17
Estimated lead time 109 business days
Only available to US customers
Only available to US customers
Known to cause cancer and reproductive harm
Known to cause cancer and reproductive harm
Classed as hazardous for shipping
Classed as hazardous for shipping
GracoRoberts P/N: 
V00257
MFR PN: 
177203400 ...
177203400 | 1772408 | 1772508 | 1962808
From $220.40
In Stock
GracoRoberts P/N: 
V00258
MFR PN: 
1772608 ...
1772608 | 1900308 | 1934108 | 510608
From $92.66
In Stock

Types of Core & Void Filling Materials

Epoxy Syntactic Foams and Compounds

Structural Void Filling Compounds

Epoxy syntactic materials incorporate lightweight fillers within a resin matrix to create compounds suited for filling cavities, supporting composite structures, and reinforcing localized areas. These materials are used in aerospace sandwich structures where controlled density, dimensional stability, and mechanical performance are important.

Structural void fillers are used to fill gaps, cavities, and irregular spaces in composite assemblies. Depending on the formulation, these materials can provide localized support and help distribute loads within bonded structures.

Select formulations are available with flame-retardant (FR) or fire, smoke, and toxicity (FST) performance characteristics, depending on the product and applicable specifications.

Core Splice Adhesive Films

Expanding Syntactic Films

Core splice films are adhesive materials designed to join adjacent sections of composite core material, including honeycomb core structures. They support core-to-core bonding during sandwich panel fabrication and help maintain continuity between core sections.

Expanding syntactic films are designed to expand during specified cure conditions, filling designated cavities or gaps within composite structures. These materials can support localized reinforcement and controlled filling in applications where a preformed film is preferred over a paste.

Applications and Performance Considerations

Honeycomb Core Splicing and Closeouts

Composite Sandwich Panel Manufacturing

Core splice adhesive films and compatible filling materials support honeycomb core bonding, edge closeouts, and transitions within composite sandwich structures. Material selection depends on core geometry, bond requirements, and processing conditions to support structural continuity and localized reinforcement.

Epoxy syntactic materials and structural void fillers are used to fill cavities, reinforce localized areas, and support interfaces between composite skins and core materials. These applications require consideration of material density, compressive properties, cure conditions, and compatibility with adjoining substrates.

Insert and Hardpoint Reinforcement

Aerospace Composite Repair and Edge Filling

Core and void filling materials can provide localized support around inserts, fittings, and load introduction points in composite assemblies. The selected material must be compatible with the surrounding core and laminate structure and meet the mechanical requirements of the application.

Compatible syntactic compounds and void fillers support approved composite repair processes involving damaged core regions, irregular cavities, and edge restoration. Material selection depends on repair geometry, processing requirements, and applicable aerospace specifications.

Material Selection and Processing Requirements

Selecting core and void filling materials requires evaluating the composite structure, application geometry, manufacturing process, and required performance of the cured material.

Key considerations include:

  • Void geometry and accessibility: Determine whether a paste, film, liquid, or cartridge format is appropriate for narrow gaps, complex cavities, and irregular surfaces.
  • Density and weight: Influence overall component weight and suitability for weight-sensitive aerospace applications.
  • Mechanical and thermal properties: Help determine suitability for structural loads, operating temperatures, and environmental conditions.
  • Viscosity and working time: Affect material placement, handling, and processing before cure.
  • Cure schedule and expansion characteristics: Define processing requirements and suitability for applications involving controlled cavity filling.
  • Material compatibility: Ensure compatibility with adjacent honeycomb cores, composite laminates, adhesives, and metallic inserts.
  • Aerospace specifications: Confirm that the selected material meets applicable program, qualification, and documentation requirements.

GracoRoberts offers core and void filling materials in multiple configurations, including cartridges, kits, sheets, and rolls, to support different manufacturing and procurement requirements.

Certification, Documentation, and Traceability

Aerospace composite manufacturing requires careful material selection and documentation to support approved fabrication and repair processes. Our portfolio includes select products associated with aerospace specifications such as BMS 5-28, BMS 5-16, and applicable manufacturer or program-specific requirements. Documentation and specification availability vary by product configuration.

Documentation and sourcing considerations include:

  • Certificates of Analysis (COA) and Certificates of Conformance (COC), where available
  • Manufacturer technical data sheets and handling instructions
  • Product-specific specification and qualification requirements
  • Lot traceability and applicable shelf life information
  • Cure conditions, storage requirements, and material compatibility

Need help selecting core or void filling materials for your composite application? Schedule a free consultation with our Composites and Adhesives Subject Matter Expert to discuss material selection and sourcing requirements.

Fibers and Fabrics FAQs

What are core and void filling materials used for in aerospace composites?

Core and void filling materials are used to fill cavities, bond core sections, and provide localized support within composite structures. Common applications include honeycomb sandwich panel fabrication, core splicing, edge filling, insert reinforcement, and approved composite repair processes.

What is the difference between syntactic foam and structural void filler?

Syntactic foam is a lightweight composite material typically made with hollow microspheres dispersed in a resin matrix. Structural void fillers include a broader range of composite resin fillers designed to fill gaps or cavities while providing specified mechanical support. Some epoxy syntactic formulations also function as structural void fillers.

How are core splice adhesive films used in composite manufacturing?

Core splice adhesive films are placed between adjacent core sections to create bonded joints during composite sandwich panel fabrication. Film selection depends on core material, bonding requirements, processing conditions, and applicable aerospace specifications.

How do I select a core filling material for honeycomb composite structures?

Core filling material selection depends on honeycomb geometry, the function of the filled area, density requirements, and compatibility with adjacent composite materials. Applications involving edge closeouts, inserts, or structural bonding may require specific compressive properties, cure conditions, and aerospace qualifications. Manufacturer technical data sheets should be reviewed to confirm suitability for the intended application.