SpanTrik is a space launch services company aiming to make space exploration more affordable by developing a fully reusable rocket, the Raven. We aim to reduce the launch cost to space, and by doing that, we can open the gates to multi-planetary civilization, and colonizing Mars will be the first step in this journey of humankind.
We are building a fully reusable rocket for launching customer payloads into space in the most reliable and affordable way.
The Name SpanTrik Originated with an Idea of combining "Space" (representing our English inspiration) with "Antriksh" (from Sanskrit), we created a unique name that reflects our diverse strengths and vision. SpanTrik symbolizes our commitment to innovation, collaboration, and pushing beyond boundaries in the space industry.
Over the years, we have designed and built multiple solid rocket motors ranging from 200 Newtons to 2.5 kN of thrust. Some of these motors were even reusable, marking significant milestones in our journey. Each motor we developed provided us with invaluable learning experiences, contributing to our robust R&D foundation. This continuous process of innovation and iteration has been instrumental in our development as a company, helping us push the boundaries of rocket technology.
we have launched over 30 high-powered rockets ranging from 100 meters to 1 kilometer for R&D purposes. These launches were conducted to understand the dynamics of rocket designing, building, manufacturing, assembly, and successfully lifting off. Each launch provided us with critical insights and data, enabling us to refine our designs and improve our manufacturing processes. This extensive hands-on experience has been crucial in developing our expertise in rocket technology and ensuring the reliability and performance of our launch vehicles.
The Eureka Lox/LNG Cryogenic Rocket Engine Development Project is a comprehensive initiative aimed at advancing the field of reusable rocket technology. The primary focus is on designing, developing, and testing a 5 kN regeneratively-cooled rocket engine powered by liquid oxygen (LOX) and liquefied natural gas (LNG). This engine development project seeks to demonstrate the feasibility of cost-effective and efficient reusable rocket.
We Conducted a series of 100+ Test of our LNG/LOX based Electrical Torch Ignitor and the Test Consisted of Cold flow and Hot test Including the Pintle Hot fire test to Ignite the main combustion chamber.
We did Series of test for our Eureka Cryogenic Rocket Engine which was able to produce 5kN, we have tested the Engine chamber Pressure from 6 to 25 Bars. we also performed quick start and Restart Capabilities.
Launch - Hover and Land Precisely.
LEAPFROGGER is a subscale demonstration of low-thrust flight that will embark on our journey to reusability. It will allow us to build the reusable rocket at a very affordable cost by reducing the development cost.
We are entering Orbit soon in 2028. The Raven is designed for launching 8 tons to LEO in fully Reusable configuration and have a capability for RTLS and The Development of Raven is parallel going on with Leapfrogger Testing all the subsystems like the Tanks Design, Sloshing Effect, Structural Integrity and the GNC system for RAVEN. it is common Structure Design with same diameter, material and tank design with same engine on both engine which make it possible to make the whole rocket Under one roof.