Tianlong-3
Tianlong-3 (, ''TL-3'') is a medium-lift orbital launch vehicle developed by the Chinese private aerospace manufacturer Space Pioneer. It is designed to be partially reusable, with the first stage capable of performing an autonomous vertical landing and being reused up to 10 times. Tianlong-3 is part of Space Pioneer's efforts to develop low-cost, reusable launch vehicles to compete in the growing commercial launch market. It aims to provide launch services for medium-sized payloads to low Earth orbit (LEO) and sun-synchronous orbit (SSO). Design First stage The first stage of the Tianlong-3 is equipped with 9 Tianhuo-12 (TH-12) liquid oxygen/kerosene engines. Each engine has a vacuum thrust of 1,350 kN, a vacuum specific impulse of 335 s, a sea-level thrust of 1,090 kN, a sea-level specific impulse of 285 s, a throttling range of 40%~110%, and a thrust-to-weight ratio of 163. The engines utilize a gas generator cycle and feature pump-fed gimbaling. The first stage ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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Space Pioneer
Space Pioneer (), also known as Beijing Tianbing Technology Co., Ltd., is a Chinese aerospace company developing reusable orbital rocket technology—both launch vehicles and liquid rocket engines—to access the market for low-cost space launch services. The company is aiming to meet launch requirements for both the Chinese national satellite internet project and also the CNSA solicitation for resupply of the Tiangong space station. The stated mission of Space Pioneer is to "pursue new breakthroughs in technology and performance, ndto select a technological path based on the needs of the commercial market to improve launch efficiency and reduce launch costs." History Space Pioneer was founded in 2019 by Kang Yonglai. Kang was the former CTO of LandSpace until 2019, when he left to establish Space Pioneer. The company completed two funding rounds in 2019, including a ZJU Joint Innovation investment, to continue liquid bipropellant engine development of the Tianhuo serie ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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TH-12
The TH-12 (, lit. ''Sky Fire 12'') is an oxidizer-rich gas-generator cycle rocket engine burning LOX and kerosene under development by Space Pioneer. The TH-12 utilizes 3D printing and has the highest target thrust among all commercial rocket engines in China. The engine features deep throttling for reusability, re-ignition, thrust vectoring, and multi-mode starters. History Space Pioneer proposed the TH-12 engine for its Tianlong-3 Tianlong-3 (, ''TL-3'') is a medium-lift orbital launch vehicle developed by the Chinese private aerospace manufacturer Space Pioneer. It is designed to be partially reusable, with the first stage capable of performing an autonomous vertical landi ... launch vehicle. Engine development was underway in December 2020, with the first gas generator test performed in September 2022. In November 2022, a full-stage developmental TH-12 engine successfully completed its first static fire test. On July 24, 2023, the TH-12 engine, in the flight configuration ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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Launch Vehicle System Tests
Launch vehicle system tests assess the readiness of a launch system to safely reach orbit. Launch vehicles undergo system tests before they launch. Wet dress rehearsals (WDR) and more extensive static fire tests prepare fully assembled launch vehicles and their associated ground support equipment (GSE) prior to launch. The spacecraft/payload may or may not be attached to the launch vehicle during the WDR or static fire, but sufficient elements of the rocket and all relevant ground support equipment are in place to help verify that the rocket is ready for flight. Propellant load tests and static fire tests may also be done on prototype rocket stages, in which case no fully assembled launch vehicle is involved, as is the case of the SpaceX Starship stages, the booster Super Heavy and the second stage Starship. Wet dress rehearsal A wet dress rehearsal is called "wet" because the liquid propellant components (such as liquid oxygen, liquid hydrogen, etc.) are loaded into the rocke ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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Comparison Of Orbital Launch Systems
This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or have attempted an orbital flight attempt as of 2024; a second list includes all upcoming rockets. For the simple list of all conventional launcher families, see: Comparison of orbital launchers families. For the list of predominantly solid-fueled orbital launch systems, see: Comparison of solid-fueled orbital launch systems. Spacecraft propulsionThere are many different methods. Each method has drawbacks and advantages, and spacecraft propulsion is an active area of research. However, most spacecraft today are propelled by forcing a gas from the back/rear of the vehicle at very high speed through a supersonic de Laval nozzle. This sort of engine is called a rocket engine. is any method used to accelerate spacecraft and artificial satellites. Orbital launch systems are rockets an ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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Comparison Of Orbital Launcher Families
This article compares different orbital launcher families (launchers which are significantly different from other members of the same 'family' have separate entries). The article is organized into two tables: the first contains a list of currently active and under-development launcher families, while the second contains a list of retired launcher families. The related article "Comparison of orbital launch systems" lists each individual launcher system within any given launcher family, categorized by its current operational status. This article does not include suborbital launches (i.e. flights which were not intended to reach LEO or VLEO). Description * Family: Name of the family/model of launcher * Country: Origin country of launcher * Manufac.: Main manufacturer * Payload: Maximum mass of payload, for 3 altitudes ** LEO, low Earth orbit ** GTO, geostationary transfer orbit ** TLI, trans-Lunar injection * Cost: Price for a launch at this time, in millions of US$ * Launches r ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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Wenchang Commercial Space Launch Site
Hainan International Commercial Aerospace Launch Co., Ltd., or HICAL, is a Chinese state-owned company that operates the Wenchang Commercial Space Launch Site, China's first commercial spaceport. Established in 2022, HICAL is the first commercially incorporated company in China to independently own and manage a spaceport. History and Launch Pads Hainan International Commercial Aerospace Launch Co., Ltd. (HICAL) was incorporated on June 2, 2022. The company is jointly funded by the Hainan Provincial Government and three state-owned aerospace contractors: China Aerospace Science and Technology Corporation, China Aerospace Science and Industry Corporation, and China Satellite Network Group. HICAL was established with a starting capital of RMB 1.5 billion. On July 6, 2022, a groundbreaking ceremony was held for the Wenchang Commercial Space Launch Site, which is China's first commercial space launch complex, and which is fully funded, constructed and operated by HICAL. Launch Com ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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Orbital Spaceflight
An orbital spaceflight (or orbital flight) is a spaceflight in which a spacecraft is placed on a trajectory where it could remain in space for at least one orbit. To do this around the Earth, it must be on a free trajectory which has an altitude at perigee (altitude at closest approach) around ; this is the boundary of space as defined by NASA, the US Air Force and the FAA. To remain in orbit at this altitude requires an orbital speed of ~7.8 km/s. Orbital speed is slower for higher orbits, but attaining them requires greater delta-v. The Fédération Aéronautique Internationale has established the Kármán line at an altitude of as a working definition for the boundary between aeronautics and astronautics. This is used because at an altitude of about , as Theodore von Kármán calculated, a vehicle would have to travel faster than orbital velocity to derive sufficient aerodynamic lift from the atmosphere to support itself. Due to atmospheric drag, the lowes ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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Reusable Spacecraft
Reusable spacecraft are spacecraft capable of repeated launch, atmospheric reentry, and landing or splashdown. This contrasts with expendable spacecraft which are designed to be discarded after use. Agencies operating reusable spacecraft aim to have lower costs and higher flight frequencies. Reusable spacecraft may be crewed or uncrewed and orbital or sub-orbital. Examples include spaceplanes such as the Space Shuttle and the Boeing X-37B, and space capsules such as the SpaceX Dragon. The Blue Origin New Shepard is an example of a sub-orbital spacecraft. History On 17 July 1962, the North American X-15 rocket plane reached an altitude of 95.9km on a sub-orbital flight. In 1963, the X-15 completed two flights above 100km. These marked the first spaceflights with a reusable vehicle. The Gemini SC-2 capsule followed, making a sub-orbital flight in 1965 and another sub-orbital flight in 1966. The first spacecraft to be reused in orbit was the Soviet VA spacecraft, a cap ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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Reusable Spaceflight Technology
Reusability is a term in computer science. Reusability may also refer to: *The quality of being fit for reuse Reuse is the action or practice of using an item, whether for its original purpose (conventional reuse) or to fulfill a different function (creative reuse or repurposing). It should be distinguished from recycling, which is the breaking down of ... * Reusable packaging See also * * {{disambiguation ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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Proposed Reusable Launch Systems
Proposal(s) or The Proposal may refer to: * Proposal (business) * Research proposal * Marriage proposal * Proposition, a proposal in logic and philosophy Arts, entertainment, and media * ''The Proposal'' (album), an album by Ransom & Statik Selektah Films * ''The Proposal'' (1957 film), an Australian television play based on Chekhov's 1890 play * ''The Proposal'' (2001 film), starring Nick Moran, Jennifer Esposito, and Stephen Lang * ''The Proposal'' (2009 film), starring Sandra Bullock and Ryan Reynolds * ''The Proposal'' (2022 film), starring Joe Joseph and Amara Raja * " La propuesta" ("The Proposal"), a short story in the 2014 Argentina anthology film ''Wild Tales'' Literature * '' Proposals (play)'', a 1997 play by Neil Simon * ''The Proposal'' (novel), 1999 and 35th book in the ''Animorphs'' series by K.A. Applegate * ''The Proposal'', alternative title of Chekhov's 1890 play ''A Marriage Proposal'' Television * ''The Proposal'' (American TV series), a 2018 realit ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |
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VTVL Rockets
Vertical takeoff, vertical landing (VTVL) is a form of takeoff and landing for rockets. Multiple VTVL craft have flown. A notable VTVL vehicle was the Apollo Lunar Module which delivered the first humans to the Moon. Building on the decades of development, SpaceX utilised the VTVL concept for its flagship Falcon 9 first stage, which has delivered over List_of_Falcon_9_and_Falcon_Heavy_launches#Launch_statistics, three hundred successful powered landings so far. VTVL technologies were first seriously developed for the Apollo program. By the '90s, development on large reliable restartable rocket engines made it possible to use the already matured technology for rocket stages. The first pioneer was the McDonnell Douglas DC-X demonstrator. After the success of the DC-X prototype, the concept was developed substantially with small rockets after 2000, in part due to incentive prize competitions like the Lunar Lander Challenge. Starting in the mid-2000s, VTVL was under intense devel ... [...More Info...]       [...Related Items...]     OR:     [Wikipedia]   [Google]   [Baidu]   |