LinkSpace did a very successful test on rocket recycling on March 27, 2019. It will support us to open the next PLAN. Thank you Dr. Robert Zubrin for being here to witness this exciting milestone. Later, NewLine Baby(RLV-T5) will undergo higher flight tests in the future.

Thanks Dr.Robert Zubrin . The Case for Mars inspires us to do our job. We are going to do the second free flight and recycle test this month. Also, there's a lot of people in China keep a close watch on Falcon Heavy's second flight and the dynamics of StarHopper.Elon Musk

Dr.Robert Zubrin Happy birthday to you🎂 生日快乐！

#ICYMI #LinkSpace successfully launches a reusable rocket to a new height

Reuters reported on LinkSpace

Reuters reported on LinkSpace

Reuters reported on LinkSpace.

Chinese space start-ups like LinkSpace are taking their first steps towards a new business model: sending tiny, inexpensive satellites into orbit at affordable prices reut.rs/2XLiu9O

On August 10, LinkSpace’s third rocket free flight test was successful in Mangai, Qinghai province. The flight time is 50 seconds, the height of flight is 300.4 meters.

300m hop test of Newline Baby reusable rocket from LinkSpace China

A new project: suborbital reusable rocket (SRV-1, Test prototype code: RLV-T6). It is a 100% reusable launch vehicle, powered by a LOX-Methane pump-fed engine.

有志者，事竟成。

Congratulations！Elon Musk one step closer to taking humans to Mars

Storm-1, the world's first LOX / methane electric pump-fed engine by LinkSpace. Full system fire test on Nov. 2nd. Thrust: 10kN (sea level) Weight: 29kg (gimbaled) / 24kg (fixed) Cycle: Electric pump-fed Pump speed: 40,000 RPM (CH4) / 35,000 RPM (LOX) Variable thrust: 30%~100%

RLV-T6 (test code, the formal product code: SRV-1) has completed a series of work including assembly, vertical test and"cold-fire test" (use LN2 instead of propellent). The rocket is expected to perform the sub-orbital reusable launch test by end of this year.

Storm 5A, LinkSpace's second pump-fed engine, completed its first full-system fire test on Sep 28th. Propellant: LOX/Mathane Sea level thrust: 5tf(expander bleed cycle) / 10tf (generator open cycle) It will be a new power system for RLV-T6 to achieve higher cost performance.

Some updates: the Storm-5A engines are undergoing more testing and iteration, the RLV-T6 rocket is fitting in with the launcher, the prototype lunar lander has completed fire test, and we're happy to see that children are interested in rockets and pay visits to our factory.