The largest variant, apparently including a third stage, would have a length of 110 meters and a takeoff mass of 4,122 tons.
The concepts would be a dramatic departure from both the expendable model of the Long March 9 and a version with a reusable first stage presented last year, with fully reusability now a goal. The frequent change in concepts however also suggests China’s plans are somewhat in flux.
The presentation, made in July, comes shortly ahead of first orbital test flights for the expendable Space Launch System and SpaceX’s fully reusable Starship.
Methane-liquid oxygen offers advantages in performance and reduces issues of soot formation and coking for purposes of reusability. The plans follow the trend of SpaceX, Blue Origin and United Launch Alliance in switching to the fuel.
It also follows a smaller two-stage methane-liquid oxygen launcher concept, apparently drawing on SpaceX’s Starship, presented by Wang Xiaojun, president of the China Academy of Launch Vehicle Technology (CALT).
The apparent switch to methalox appears sudden. China’s propulsion institutes, under the state-owned conglomerate the China Aerospace Science and Technology Corporation (CASC), have however long been working on methane engines, making a change of plans somewhat feasible.
A smaller five-meter-diameter reusable rocket presented by Long could potentially be intended to replace a number of aging hypergolic rockets, as well as more recent kerosene-fueled Long March rockets which have become operational over the last decade.
Chinese commercial launch companies Landspace and iSpace have been developing methane-liquid oxygen launchers in recent years, possibly with help of military-civil fusion national strategy which facilitates transfer of restricted technologies.
Landspace is set to attempt its first launch on the methalox Zhuque-2 in the near future from Jiuquan spaceport. Competitor iSpace is also preparing to conduct hop tests with a methalox first stage test article for its reusable Hyperbola-2 rocket at Jiuquan.
Long March 9 evolution
While various figures have been published, the original, expendable Long March 9 is expected to be around 103 meters long, feature a 10-meter-diameter core and have a mass at liftoff of 4,140 metric tons, and be capable of lifting 140 tons to Low Earth orbit or 50 tons to trans-lunar injection.
Dual nozzle 500 ton-thrust kerosene-liquid oxygen (YF-130) engines will power the first stage and boosters, 220-ton-thrust liquid hydrogen-liquid oxygen staged combustion cycle (YF-90) engines for the second stage, with significant progress already made on both. Vacuum-optimized hydrolox engines would power the third stage.
The reusable first stage version presented in 2021 would switch to a first stage using 16 clustered 360-ton-thrust kerolox engines and no side boosters. 120-ton-thrust hydrolox engines would be used for the second and third stages.
The largest variant of the Long March 9 in Long’s new lecture featuring the fully reusable concepts would have a 10.6-meter-diameter, a length of 110 meters and takeoff mass of 4,122 tons, matching the capabilities of the earlier plans.
A more economical, reusable version of the Long March 9 could be ready to support a proposed space-based solar power program in geostationary orbit.
China is also developing a three-stage heavy-lift rocket designed to be capable of sending Chinese astronauts to the moon. A two-stage version for low Earth orbit could have its first flight in 2026.
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