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  2. Hydroxyl-terminated polybutadiene - Wikipedia

    en.wikipedia.org/wiki/Hydroxyl-terminated_poly...

    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 the specific impulse of the black powder propellant used in most smaller rocket motors. HTPB is also used as a hybrid rocket fuel. [2]

  3. Polybutadiene acrylonitrile - Wikipedia

    en.wikipedia.org/wiki/Polybutadiene_acrylonitrile

    Polybutadiene acrylonitrile (PBAN) [1] copolymer, also noted as polybutadiene—acrylic acid—acrylonitrile terpolymer [2] is a copolymer compound used most frequently as a rocket propellant fuel mixed with ammonium perchlorate oxidizer. [3] It was the binder formulation widely used on the 1960s–1970s big boosters (e.g., Titan III and Space ...

  4. AJ-60A - Wikipedia

    en.wikipedia.org/wiki/AJ-60A

    AJ-60A is a solid fueled rocket burning HTPB-based composite solid propellant. [8] The casing is composed of a graphite-epoxy composite, and the engine throat and nozzle are made of carbon-phenolic composite.

  5. Ammonium perchlorate composite propellant - Wikipedia

    en.wikipedia.org/wiki/Ammonium_perchlorate...

    Ammonium perchlorate composite propellant (APCP) is a solid rocket propellant. It differs from many traditional solid rocket propellants such as black powder or zinc-sulfur , not only in chemical composition and overall performance but also by being cast into shape, as opposed to powder pressing as with black powder.

  6. P160C - Wikipedia

    en.wikipedia.org/wiki/P160C

    Propellant: HTPB / AP / Al: The P160C is a solid-fuel rocket engine designed for use as the first stage of the Vega-E and as the boosters of the Ariane 6 Block 2 ...

  7. Hybrid-propellant rocket - Wikipedia

    en.wikipedia.org/wiki/Hybrid-propellant_rocket

    Generally, the liquid propellant is the oxidizer and the solid propellant is the fuel because solid oxidizers are extremely dangerous and lower performing than liquid oxidizers. Furthermore, using a solid fuel such as Hydroxyl-terminated polybutadiene (HTPB) or paraffin wax allows for the incorporation of high-energy fuel additives such as ...

  8. Zefiro (rocket stage) - Wikipedia

    en.wikipedia.org/wiki/Zefiro_(rocket_stage)

    The propellant of all Zefiro models is HTPB 1912 with a nominal composition of 19% of aluminium powder, 69% of ammonium perchlorate with 12% of hydroxyl-terminated polybutadiene binder. [ 15 ] Zefiro 23 and Zefiro 9A , where the number represent the intended propellant weight at design phase, are used respectively as second and third stage of ...

  9. Solid-propellant rocket - Wikipedia

    en.wikipedia.org/wiki/Solid-propellant_rocket

    A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer). The earliest rockets were solid-fuel rockets powered by gunpowder . The inception of gunpowder rockets in warfare can be credited to the ancient Chinese, and in the 13th century, the Mongols played a pivotal role in ...