The invention relates to novel series of
hydrogen peroxide thrust chambers used for rockets and airships. The novel series of
hydrogen peroxide thrust chambers comprise micro
attitude control types, small-sized
orbit control types, middle-sized
acoustic cavity types, large-sized partition types and ultra-large types; industrial 79.1%-84.9%
hydrogen peroxide is used as an
oxidizing agent and a regenerative
coolant; a non-toxic homogeneous miscible fuel (NHMF),
kerosene or
liquid hydrogen is taken as a fuel; non-toxic storable components account for 95%-100% of a
propellant, so that the use is convenient; the
decomposition rate of a catalyst
bed is controlled within 75%-95%, the development and service life prolonging of the catalyst
bed are facilitated; and novel structures such as a high strength head, a
regenerative cooling nineteen-zone partition, a semi-opening
acoustic cavity, a gas-liquid impinging
injector, a multihole
conical shell are adopted. According to the novel series of
hydrogen peroxide thrust chambers used for rockets and airships, the
combustion temperature,
decomposition temperature and
regenerative cooling temperature rise are low, so that the working conditions are improved at lot; besides, the density-
specific impulse is higher, the propulsive performance is better, and therefore the thrust chambers are applicable to boosters, first-stage and second-stage engines as well as first-stage core engines, which are capable of being used for over 25 times, of novel manned Moon and
Mars landing rockets and airships.