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Hydroxyl-terminated polybutadiene

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(Redirected fromHTPB)
Chemical compound

Hydroxyl-terminated polybutadiene (HTPB) is anoligomer ofbutadiene terminated at each end with ahydroxylfunctional group. It reacts withisocyanates to formpolyurethane polymers.

HTPB is a translucent liquid with a color similar to wax paper and a viscosity similar to corn syrup. The properties vary because HTPB is amixture rather than a purecompound, and it is manufactured to meet customers' specific requirements. A typical HTPB is R-45HTLO.[1] This product consists of oligomeric units typically containing 40–50 butadiene molecules bonded together, with each end of the chain terminated with a hydroxyl [OH] group:

R-45HTLO has afunctionality of 2.4-2.6, which means that there is (approximately) one additional hydroxyl group located along the chain for every two oligomeric units. This provides side-to-side linkage for a stronger cured product. HTPB is usually cured by anaddition reaction with di- or poly-isocyanate compounds.

Uses

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Materials production

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Polyurethanes prepared from HTPB can be engineered for specific physical properties; polyurethanes may be highly elastic or tough and rigid. Some products include: rigid foam insulation panels; durable elastomeric wheels and tires (used forroller coasters,escalators,skateboards, etc.); automotive suspensionbushings; electrical potting compounds; high-performanceadhesives; surface coatings and surface sealants;synthetic fibers (e.g.,Spandex);carpet underlay; hard-plastic parts (e.g., for electronic instruments).

Rocket propellant

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An important application of HTPB is insolid rocket propellant. It binds theoxidizing agent, fuel and other ingredients into a solid but elastic mass in most composite propellant systems. The cured polyurethane acts as a fuel in such mixtures. For example, HTPB is used in all 3/4 stages of the JapaneseM-5 launch vehicles and in 1/3 stages of IndianPSLV launch vehicle.JAXA describes the propellant as "HTPB/AP/Al=12/68/20", which means, proportioned by mass, HTPB plus curative 12% (binder and fuel),ammonium perchlorate 68% (oxidizer), andaluminum powder 20% (fuel).

Similar propellants, often referred to as APCP (ammonium perchlorate composite propellant) are used in larger model rockets. A typical APCP propellant mixture produces 2–3 times thespecific impulse of theblack powder propellant used in most smaller rocket motors.

HTPB is also used as ahybrid rocket fuel.[2] With N2O (nitrous oxide, or "laughing gas") as the oxidizer, it is used to power theSpaceShipTwo hybrid rocket motor developed bySpaceDev.[3] The land speed record attemptBloodhound SSC was to have used HTPB with ahigh-test peroxide oxidizer, but that plan was altered in 2017.

See also

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References

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  1. ^http://www.crayvalley.com/docs/TDS/poly-bd-r-45htlo.pdfArchived 2016-02-16 at theWayback Machine[bare URL PDF]
  2. ^Sutton, George Paul; Biblarz, Oscar (2010).Rocket propulsion elements (8th ed.). Hoboken, N.J: Wiley. pp. 595–599.ISBN 978-0-470-08024-5.
  3. ^"SpaceDev Hybrid Propulsion". SpaceDev. Archived fromthe original on 2007-11-05. Retrieved2008-07-24.

External links

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