Overview
This transformative project seeks to enhance the gallery’s infrastructure, accessibility, and exhibition spaces while preserving its rich cultural heritage.

Project One commenced in 2021 with support from Bharat Forge’s Aerospace Department. The project’s objective was to build a reusable kerosene-liquid oxygen rocket engine. The detailed concept was presented by Manan to the Bharat Forge Aerospace Team in January. Vinith and Kalyani joined the team in April and August, respectively.
Over the following months, the team delved into rocket fundamentals and identified challenges in rocket engine design. They also encountered supply-side issues and highlighted technology restrictions, such as ITAR regulations. During the engine’s development, the team engaged with various international teams from Ukraine to the US. Through this process, the team discovered that propulsion technology in India is primarily developed by government agencies. Consequently, the Indian space industry either imports technologies or runs expensive development programs.
TEXT
Recognizing the absence of a propulsion company focused on developing necessary propulsion systems and subsystems, the team began working to address this gap.
During our journey of over two years, they identified a compelling business case for their work. We saw an opportunity to provide propulsion technology for Indian and similar markets while leveraging the existing supply chain that ISRO has developed over many decades. Armed with this knowledge, we formed Thrustworks Dynetics on 22/02/23.
Create anything
Thrust
✦
The company is currently focused on the development of ANYA, a semi-cryogenic rocket engine with a thrust of 20 kN.
Propellent
✦
Kerosene and Liquid oxygen (KereLOx)
Engine Cycle
✦
The utilization of open cycle gas generators will guarantee simplicity and enable individual subsystem testing.
Thrust ToWeight Ratio
✦
A TWR greater than 100 is desired for this engine, which can be achieved through weight reduction. The target weight for the engine is set below 20Kg, as outlined in the detailed mass budget section.
we are passionate about the cutting edge designs shaping our world today.
Our Services

Preliminary Design Report (PDR)
Our PDR offers the entire engine design at a fraction of the cost traditionally charged. Additionally, we offer accelerated development time, providing agility to the customer to keep up with changing requirements as the development progresses.

Critical Design Report (CDR)
Our Critical Design report includes comprehensive testing of our proven subsystem designs, which have been fine-tuned to meet the specific requirements of our customers. By utilizing 3D printing technology, we can achieve faster iteration times at a lower cost, allowing us to provide an efficient and cost-effective solution to our customers’ needs.

Engine Prototype:
Engine Prototype:
Our company specializes in delivering high-speed engine development for our clients. Our engines undergo a series of rigorous integrated static tests and operationalization tests to ensure the highest level of quality. Based on our proven design, our prototypes offer a more cost- effective and efficient solution for our customers, resulting in faster development and iteration times.

Engine Production:
Engine Production
Our company offers comprehensive engine production
services that cater to the specific launch cadence of a
particular vehicle, with a primary goal of reducing per unit
engine costs. Additionally, we provide ongoing engine
improvement services over the entire lifecycle of the program
at a low cost rocket engine.

FUTURE SCOPE
TWD is formed to build advanced propulsion systems with a vision to one day create an engine called as High Thrust High Impulse Engine (HTHI). HTHI engine will have the efficiency of an electric propulsion system but the thrust of a chemical rocket. However, before we take steps into creating such a system we need to solve immediate problems such as access to rocket engines for commercial application and ultra small scale power generation system.
