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MP55S
 
 
  
A graphite combustion modified flexible polyether polyurethane foam which has been specially designed for use in aircraft seating.
 
 
 
 
PRODUCT TECHNICAL DATA

      TYPICAL PHYSICAL PROPERTIES
 Physical properties are measured using test methods described in the
 BS4443 series and BS EN ISO 845:1995.

 Nominal piece density range  53-58 kg/m3

 Nominal hardness range   70-100 N

 Nominal CLD Hardness (40%)  1.9-3.0 kPa

 Nominal tensile strength   60 kPa min.

 Nominal elongation at break  100% min.

 FOAM CLASSIFICATION (BS3379)
 Foam type CMHB  : Combustion Modified High Resilience
      Slabstock
 Nominal Classification : S

 FLAMMABILITY CHARACTERISTICS
 Capable of meeting the following requirements :
 1. ATS-1000.001/ABD 0031 Airbus Industrie technical specification
  regarding smoke and toxicity.
 2. FAR 25.853 (a) Amendment 25-72 Part 1, Appendix F –
  Vertical burn test.
 3. FAR 25.853 (c) Amendment 25-72 Part 2, Appendix F –
  Kerosene burn test.
 
 Meets the requirement of a maximum weight loss of 10% when used in
 combination with higher density MP or DAX grades and a typical 90/10
 [90% Wool/ 10% Polyamide] cover.

 N.B. MP55S is capable of meeting the 10% maximum weight loss without a
 cover.

 
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