The topic of this article may not meet Wikipedia's notability guidelines for companies and organizations .(November 2024) |
Company type | Private |
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Industry | Aerospace |
Founded | 2022 |
Founder |
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Headquarters | , |
Products | |
Services | Launch vehicles |
Website | www |
Ethereal Exploration Guild Private Limited is an Indian startup based in Bengaluru developing fully reusable vertical landing medium-lift space launch system at reduced cost and cut launch timeframes. [1] [2] Founded in 2022, the company is currently developing India's largest private rocket engine facility in the southern state of Tamil Nadu. [3] The launch vehicle 'Razor Crest Mk-1' will be able deliver up to eight-tonnes to low earth in fully reusable configuration. [3]
The startup was founded by; Manu J Nair (Chief Executive Officer) who was briefly a part of the Gaganyaan, the manned spaceflight program of the Indian space agency, Shubhayu Sardar (Chief Operations Officer) a former ISRO engineer and graduate of Indian Institute of Space Science and Technology and Prashanth Sharma (Chief Technology Officer) an aerospace engineer. [1] It has raised US$ 5 million seed funding. [3] [4]
The mark-one variant of the launch system features an absolute reusable configuration in which both the booster and the upper stage are recoverable. The recovery of the upper stage comes with a crucial issue of fending off reentry heat, the startup intends to develop a new rocket engine cycle along with a deployment system to redirect the heat built up throughout the reentry phase. This will allow the system to operate efficiently in both atmosphere and vacuum. Thereby the launch system will be able to achieve pinpoint landing compared to the larger target landing zones in the case of traditional ballistic reentry. [3]
The rocket will be capable of launching up to 8 tonnes to low earth in fully reusable configuration and almost 24.8 tonnes to low earth in an expendable configuration. [1]
Once developed, the 'Stallion' as claimed will be the most powerful operational liquid rocket engine outside North America. Powered by RP1/LOX propellent, it will be able to produce a peak thrust of 925 kN. It features gas generator feed cycle and will have a peak specific impulse of 295 seconds at sea level and 330 seconds in a vacuum. 'Razor Crust Mk-1' will house nine of this engine. [1]
S.No | Date / time (UTC) | Rocket Configuration | Launch site | Payload | Orbit | Customer | Status |
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Remarks | |||||||
1. | NET 2026 | Technology Demonstrator Vehicle (TDV) | TBA | TBA | LEO | TBA | Planned |
The 35-meter tall and 2.5-meter wide technology demonstrator launch vehicle with a 1.2-ton capacity to 400 km low earth orbit. It will feature the same engine type as a full-scale launch vehicle, but in a smaller count. The launch is intended to verify the telemetry data and flight software for its future commercial launches. |
A spacecraft is a vehicle that is designed to fly and operate in outer space. Spacecraft are used for a variety of purposes, including communications, Earth observation, meteorology, navigation, space colonization, planetary exploration, and transportation of humans and cargo. All spacecraft except single-stage-to-orbit vehicles cannot get into space on their own, and require a launch vehicle.
An expendable launch system is a launch vehicle that can be launched only once, after which its components are either destroyed during reentry or discarded in space. ELVs typically consist of several rocket stages that are discarded sequentially as their fuel is exhausted and the vehicle gains altitude and speed. As of 2024, fewer and fewer satellites and human spacecraft are launched on ELVs in favor of reusable launch vehicles. However, there are many instances where a ELV may still have a compelling use case over a reusable vehicle. ELVs are simpler in design than reusable launch systems and therefore may have a lower production cost. Furthermore, an ELV can use its entire fuel supply to accelerate its payload, offering greater payloads. ELVs are proven technology in widespread use for many decades.
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Fuji (ふじ) was a crewed space capsule proposed by Japan's National Space Development Agency (NASDA) Advanced mission Research center in December 2001. The Fuji design was ultimately not adopted.
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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, although many partially reusable spacecraft discard some kind of expendable module before reentry and recovery.
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