Deacon Rocket Wrap - Deacon High Temperature Sealants

Engineered Carbon Fiber Composite Wrap

Deacon® Rocket Wrap® is a carbon fiber composite wrap featuring a proprietary weave that has been tested in the lab and field to withstand extreme temperatures and pressures.

Deacon Rocket Wrap offers a comprehensive carbon fiber wrap solution for a wide variety of industrial applications. The heavy industrial carbon fiber offers unique repair properties, resulting in minimal to zero downtime, no demolition, and no new permitting.

Deacon Rocket Wrap has been tested to hold up to extreme pressures and temperatures.

ASME PCC-2 and ISO 24817 Certified.

Conforms to:
- API-653
- DOT
- ASME B31

Rocket Wrap Sell Sheet

Seal Wrap Sell Sheet

Rocket Wrap Flyer

Want to Speak to a Team Member About Deacon Rocket Wrap?

Why Choose Rocket Wrap?

ASME PCC-2 and ISO 24817 Certified
Low Thermal Expansion
Extreme Chemical Resistance
High Tensile Strength
High Temperature Tolerance
High Strength-to-Weight Ratio
Substantial Cost-Savings of 80% vs. Replacement
Permanent Solutions
Custom Engineered Solutions
Conforms to Odd Geometry
Specially Formulated Proprietary Blend Epoxy
Reinforces Structures Beyond Original Capacity
Mitigates Environmental Damage due to Material Loss
Rocket Wrap FAQ

Target Industries

Petrochemical
Refinery
Pipeline
Manufacturing/Industrial
Steel
Pulp & Paper
Power Generation
Construction
Marine
Transportation

Applications

The repair solution for internal and external corrosion, erosion, stress cracking, direct leaks, soft spots, microbial induced corrosion (MIC), and general industrial leak repair.

Process Piping
Tanks
Pipelines
Silo Reinforcement & Repair
Concrete Structural Repair
Support Columns & Beams

Product Line

LEARN MORE about each product listed below by clicking on Product Name.

Chemical Compatibility Chart

Rocket Wrap TDS

PRODUCT	TDS	SDS
Deacon Rocket Repair Kit	Rocket Repair Kit TDS English	Rocket Fabric SDS English Rocket Saturant (Part 1 Resin) SDS English Rocket Saturant (Part 2 Hardener) SDS English Rocket Primer (Part 1 Resin) SDS English Rocket Primer (Part 2 Hardener) SDS English
Deacon Rocket Fabric	Rocket Fabric TDS English	Rocket Fabric SDS English
Deacon Rocket Saturant	Rocket Saturant TDS English	Rocket Saturant (Part 1 Resin) SDS English Rocket Saturant (Part 2 Hardener) SDS English
Deacon Rocket Filler	Rocket Filler TDS English	Rocket Filler (Part 1 Resin) SDS English Rocket Filler (Part 2 Hardener) SDS Englis
Deacon Rocket Primer	Rocket Primer TDS English	Rocket Primer (Part 1 Resin) SDS English Rocket Primer (Part 2 Hardener) SDS English
Deacon UV Top Coat	UV Top Coat TDS English	UV Top Coat (Part 1) SDS English UV Top Coat (Part 2) SDS English
Deacon Booster Kit	Booster Kit TDS English	Booster Powder SDS English Rocket Saturant (Part 1 Resin) SDS English Rocket Saturant (Part 2 Hardener) SDS English
Deacon Jacket Wrap	Jacket Wrap TDS English	Jacket Wrap SDS English
Deacon Diamond Putty	Diamond Putty TDS English	Diamond Putty SDS English
Deacon Seal Wrap Deacon Seal Wrap FC Deacon Seal Wrap SC	Seal Wrap TDS English Seal Wrap FC TDS English Seal Wrap SC TDS English	Seal Wrap SDS English Seal Wrap FC SDS English Seal Wrap SC SDS English

Rocket Wrap FAQ

What is the maximum temperature rating for Rocket Wrap?

The heat distortion temperature (HDT) for the composite system is 514°F (268°C). In accordance with Section 401-3.4.2 of PCC-2, 27°F (15°C) is subtracted from the HDT for Type A (non-leaking) repairs. On Type B (leaking / defect) repairs, 45°F (25°C) is subtracted from the HTD. Our engineered design packages document that the system can handle 487°F / 253°C (Type A) or 469°F / 243°C (Type B).

Where was the PCC-2 qualification testing performed?

Stress Engineering Services in Houston, TX.

How do you certify installers?

We perform In-person classroom training followed by hands on instruction. Each installer is required to wrap a piece of pipe with a defect that is ultimately sent to Stress Engineering Services for pressure testing.

Do you charge for in-person training?

What temperature(s) were the chemical compatibility tests performed at?

Chemical compatibility was performed in the lab at 77F (25C) and/or in the field up to the maximum operating temperature of the product(s). Our experience with two-part epoxies goes back to 1988

Which substrate material(s) has qualification testing been performed for (Mandatory Appendix 405-IV data)?

Rocket Wrap was qualified on carbon steel. Additional testing will be performed on stainless steel in the near future.

What is the fiber orientation pattern for the fabric? Are any directions weighted more than others?

The fabric is composed of 12K and 6K tows in a biaxial orientation. Eight yarns per inch +/-0.5 for both sizes.

Are there any hold points for applications where fiber orientation is critical? (E.g. patches, large OD repairs, etc.)

Our definition of hold points are pauses in the procedure to check conditions pre wrap, during wrap and post wrap. These topics are part of our training that is required to use our product. Additional hold points are part of specific instructions for customer requested full design packages if needed for critical applications. In these situations, our Engineering Department is fully engaged with the design and planning activities with the customer and selected applicator. The typical wrapping applications do not require additional hold points other than what is routine for providing full and correct preparation for wrapping.

How are large open times between surface preparation and first application handled?

Work times for the saturant, filler, and primer are dependent on the atmospheric conditions, substrate temperature, and volume of product being mixed. Guidelines pertaining to application temperature, pot life, and tack free times are listed on the TDS.

I may have missed it but I didn’t see any cure schedules. Could you either point me in the right direction or provide the relevant documentation?

Please refer to the TDS for additional information regarding curing. The curing for the epoxy is very straightforward, mix appropriate ratios of part A and B, mix thoroughly, saturate and apply fabric as per training, apply compression wrap, allow time for full cure. Remember that environmental conditions will fully dictate cure speed and ultimate hardness.

When designing a repair, is there a check for the possibility of delamination?

PCC-2 is the standard followed for all calculations and related conditions for performing a wrap repair. See section 401-4.7 Live Repairs. If a customer has a situation where they request this specific examination, we would be happy to explore this with them. This is not a routinely used formula.