Projects
Build Beyond.
We don't follow trends—we engineer what's next. Precision, performance, and power—built for those who aim higher.
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Total Projects
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Completed
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Progress

ROCKETS • DRONES • PLANES

TIVRA L-1380
Motor
Completed
TIVRA L-1380
The TIVRA L-1380 is a high-performance solid rocket motor delivering up to 4000 N of peak thrust with a total impulse of 4000 Ns and a 2.5-second burn time. Designed for reliable and powerful propulsion, it is well-suited for advanced experimental rocketry, research testing, and aerospace demonstration missions.
Progress100%
09/21/25
10/10/25

Technologies:

Solid Composite Propellant TechnologyAdvanced Grain Geometry DesignPrecision Nozzle EngineeringStatic Test–Validated Thrust Profiling+1
TIVRA K-560
Motor
Completed
TIVRA K-560
The TIVRA K-560 is a compact solid rocket motor delivering up to 1030 N of peak thrust with a total impulse of 1960 Ns and a 3.5-second burn time. Designed for reliable and stable propulsion, it is ideal for experimental rocketry, student programs, and research missions requiring moderate-thrust, extended-burn performance.
Progress100%
09/16/25
09/20/25

Technologies:

Solid Composite Propellant TechnologyInternal Thermal Insulation SystemHigh-Temperature Nozzle MaterialsStatic Test–Validated Thrust Profiling
Thrust Vector Control
Equipment
Completed
Thrust Vector Control
Thrust Vector Control
Progress100%
08/01/25
08/21/25

Technologies:

Control Systems
MEGH 1K23
Rocket
Completed
MEGH 1K23
High-altitude research rocket with advanced telemetry systems and payload capacity for atmospheric research.
Progress100%
07/28/25
10/15/25

Technologies:

Solid PropulsionAdvanced TelemetryGPS NavigationRecovery System+4
Bhishma
Equipment
Completed
Bhishma
Bhishma
Progress100%
05/29/25
05/31/25

Technologies:

Mechanical
VAJRA
Rocket
Completed
VAJRA
VAJRA
Progress100%
02/19/25
06/10/25

Technologies:

Mechtronics
TIVRA K-925
Motor
Completed
TIVRA K-925
The TIVRA K-925 is a mid-range solid rocket motor delivering up to 1550 N of peak thrust with a total impulse of 2500 Ns and a 2.7-second burn time. It is designed to provide reliable, high-performance propulsion for experimental rocketry, student programs, and aerospace research missions.
Progress100%
02/16/25
06/10/25

Technologies:

Solid Composite PropulsionOptimized Grain DesignThermal ProtectionHigh-Temperature Nozzle+1
Mechanical Recovery
Rockets
Completed
Mechanical Recovery
Mechanical Recovery
Progress100%
10/07/24
10/30/24

Technologies:

Mechatronics
GATI E-30
Motor
Completed
GATI E-30
The GATI E-30 is a compact solid rocket motor delivering up to 42 N of peak thrust with a total impulse of 30 Ns and a 1-second burn time. Designed for small experimental rockets and educational applications, it provides reliable short-duration propulsion in a lightweight form factor.
Progress100%
09/09/24
10/06/24

Technologies:

Solid Composite PropulsionPrecision Grain DesignCompact CasingThermal Protection+1
Atomiser
Equipment
Completed
Atomiser
Atomiser
Progress100%
02/06/24
08/21/25

Technologies:

Pressure Fed System
CanSat
Equipment
Completed
CanSat
CanSat
Progress100%
03/05/24
04/15/24

Technologies:

pcb
CubeSat
Equipment
Completed
CubeSat
CubeSat
Progress100%
12/01/23
01/10/24

Technologies:

PCB
TR -1000
Rocket
Completed
TR -1000
The TR-1000 is a lightweight experimental sounding rocket designed to carry a 1 kg payload to an altitude of up to 1 km. With an all-up weight of 5.5 kg and a cardboard-based airframe, the TR-1000 serves as a low-cost platform for technology demonstration, student research, and CanSat deployment missions. The vehicle is currently ground-tested and configured for unguided flight.
Progress100%
10/15/23
12/02/23

Technologies:

Lightweight StructuresI-Class PropulsionFlight ComputerMechanical Deployment+1
Static Thrust Bench
Equipment
Completed
Static Thrust Bench
stb
Progress100%
08/10/23
10/05/23

Technologies:

stb
GATI F-20
Motor
Completed
GATI F-20
The GATI F-20 is a compact solid rocket motor featuring a CPVC casing, delivering up to 53.18 N of peak thrust with a total impulse of 72 Ns and a 3-second burn time. It is designed for small experimental rockets, student projects, and propulsion testing where affordability and reliability are essential.
Progress100%
04/02/23
04/21/23

Technologies:

Solid Composite PropulsionCPVC CasingThermal ProtectionPrecision Grain Design+1

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