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Park Aerospace F-552

Chemical Family
Phenols & Phenolics

Park’s F-552 is a high purity silica filled phenolic resin coated on high strength grade silica fabric. F-552 is used in the manufacture of intermediate temperature ablative rocket nozzles, heat shields, and combustion chambers in highly oxidative environments.

Product families

Applications

Automotive & Transportation — Transportation
  • Aerospace & Aviation

Product Families

Composite Materials — Prepregs & Molding Compounds
  • Thermoset Prepregs

Other characteristics

Functions
Prepreg
Polymer Name
Phenolic Compound
Processing Methods
Compression Molding, Prepreg Processing
Reinforcement Material
Other Reinforcement Material
Markets
Automotive & Transportation
Technology
Composite Materials
Product Forms

Available in Broadgoods, Chopped Molding Compound and Bias Tape; Solution coated fabrics up to 38" inches wide; Compatible with Autoclave or Press Molding processes

Fillers Included
Silica
Quality Standards
  • MIL-R-9299C
  • WS-21053
Material Features
Ablation Resistant
Prepreg Storage Life
Out Life
30 days @ 75°F
Shelf Life
6 months @ 40°F (dry)
Benefits and Features

Provides a combination of high-strength and ablative properties for demanding applications.; Low thermal expansion; Good Tack and Drape properties; Conforms to WS-21053; Resin conforms to MIL-R-9299

Applications and Qualifications
  • Rocket Nozzles
  • Combustion Chambers
  • Heat Shields
  • Rocket Motor Throat Sections
Composite Materials Functions
Prepreg
Composites Processing Methods
  • Compression Molding
  • Prepreg Processing
Autoclave Cure Cycle

Apply 24"Hg vacuum (minimum) for 1 hour before beginning heat cycle; Apply 10 psi autoclave pressure; Raise product temperature from RT to 250°F at 2 - 5°F/min; Increase autoclave pressure to 40psi, vent vacuum at 15 – 20 psi; Hold product at 250 ± 5°F for 30 minutes; Raise product temperature to 325 ± 5°F at 2 - 5°F/min; Hold product at cure temperature for 60 – 90 minutes; Cool to 150°F at no at no more than 8°F/min prior to releasing autoclave pressure

Press Cure Cycle (Chopped Molding Compound)
  • Apply 1,000 - 2,000 psi pressure during cure
  • Cure product at 325°F for 90 – 120 minutes

Technical data

Table 1 of 2

9 rows
CharacteristicValueUnitMethod
Nominal Prepreg Weight30oz/sqyd—
Resin Solids Content29 - 36%—
Filler Content4 - 11%—
Resin Flow (325°F, 150 psi)10 - 20%—
Volatiles (325°F, 10 min)3 - 5.5%—
Nominal Cured Ply Thickness0.021——
Barcol Hardness70—ASTM-D-2583
CTE - With Ply (75 - 340°)5.8μin/inꞏºFASTM-E-831
CTE - Across Ply (75 - 340°)18.8μin/inꞏºFASTM-E-831

Table 2 of 2

16 rows
CharacteristicValueUnitMethod
Specific Gravity1.8g/ccASTM-D-792
Specific Heat0.26BTU/lb°FASTM-C-351
Thermal Conductivity - With Ply (250°F)0.29BTU/ft2-hr°FASTM-C-177
Thermal Conductivity - Across Ply (250°F)0.4—ASTM-C-177
Thermal Diffusivity - With Ply (250°F)0.014ft2/hrASTM-C-177
Thermal Diffusivity - Across Ply (250°F)0.012—ASTM-C-177
Cure Cycle (325°F)1000psi—
Tensile Strength - Dry (75°F)16.48KsiASTM-D-638
Tensile Modulus - Dry (75°F)1.25MsiASTM-D-638
Tensile Strength - Dry (90° 75°F)16.5KsiASTM-D-638
Tensile Modulus - Dry (90°C 75°F)1.3MsiASTM-D-638
Compressive Strength - Dry (75°F)60.8KsiASTM-D-695

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