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.