Launch Solutions
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Fully Customisable
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Rapid Constellation Deployment
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Non-Pyrotechnic HDRM
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Side Volume for Solar Panels
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1 - 32 kg Payload
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Up to 16U Volume Available
Satellite Orbital Deployers Range
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CubeSat Form Factor
1U, 2 x 0.5U, etc.
Deployer Mass
3.2 kg
Total CubeSat Mass
2 kg
Side Volume
Up to 15 mm on all sides
Pointing Accuracy
Up to 0.1°
DSOD-1U
Dhruva Space Satellite Orbital Deployer 1U
- TRL 9
- Multiple CubeSat configurations
- Space-Qualified, pre-qualified, assembled (Mechanical and Electrical) and ready for payload integration
- Non-Pyrotechnic Hold-Down and Release Mechanism (HDRM)
- Onboard Telemetry Sensors included for Deployment Confirmation and Ejection Velocity Measurement
Get a quote
CubeSat Form Factor
1U, 1.5U, 2U, 3U
Deployer Mass
5.8 kg
Total CubeSat Mass
6 kg
Side Volume
Up to 15 mm on all sides
Ejection Velocity
<2 m/s
DSOD-3U
Dhruva Space Satellite Orbital Deployer 3U
- TRL 9
- Multiple CubeSat configurations
- Space-Qualified, pre-qualified, assembled (Mechanical and Electrical) and ready for payload integration
- Non-Pyrotechnic Hold-Down and Release Mechanism (HDRM)
- Reconfigurable design to accommodate Hosted Payload
- Onboard Telemetry Sensors included for Deployment Confirmation and Ejection Velocity Measurement
Get a quote
Switch to Composite
Switch to Metal
CubeSat Form Factor
1U, 3U, 6U and XL sizes for each as per standard CDS dimensions
Deployer Mass
8.3 kg
Total CubeSat Mass
Up to 2 kg per U
Side Volume
Up to 15 mm on all sides
Ejection Velocity
<2 m/s
DSOD-6U
Dhruva Space Satellite Orbital Deployer 6U
- TRL 9
- Multiple CubeSat configurations
- Space-Qualified, pre-qualified, assembled (Mechanical and Electrical) and ready for payload integration
- Non-Pyrotechnic Hold-Down and Release Mechanism (HDRM)
- Onboard Telemetry Sensors included for Deployment Confirmation and Ejection Velocity Measurement
Get a quote
CubeSat Form Factor
1U, 3U, 6U and XL sizes for each as per standard CDS dimensions
Deployer Mass
5.08 kg
Total CubeSat Mass
Up to 2 kg per U
Side Volume
Up to 15 mm on all sides
Ejection Velocity
<2 m/s
DSOD-6U Composite
Dhruva Space Orbital Deployer 6U Composite
- Multiple CubeSat configurations
- Pre-Qualified, assembled (Mechanical and Electrical) and ready for payload integration
- Non-Pyrotechnic Hold Down and Release Mechanism (HDRM)
- Onboard Telemetry Sensors included for Deployment Confirmation and Ejection Velocity Measurement
Get a quote
CubeSat Form Factor
1U, 1.5U, 2U, 3U, 6U, 12U
Deployer Mass
7.9 kg
Total CubeSat Mass
24 kg
Side Volume
Up to 15 mm on all sides
Ejection Velocity
<2 m/s
DSOD-12U Composite
Dhruva Space Satellite Orbital Deployer 12U Composite
- Multiple CubeSat configurations
- Pre-Qualified, assembled (Mechanical and Electrical) and ready for payload integration
- Non-Pyrotechnic Hold-Down and Release Mechanism (HDRM)
- Reconfigurable design to accommodate Hosted Payload
- Onboard Telemetry Sensors included for Deployment Confirmation and Ejection Velocity Measurement
Get a quote
CubeSat Form Factor
1U, 1.5U, 2U, 3U, 6U, 12U, 16U
Deployer Mass
16 kg
Total CubeSat Mass
32 kg
Side Volume
Up to 15 mm on all sides
Ejection Velocity
<2 m/s
DSOD-16U Composite
Dhruva Space Satellite Orbital Deployer 16U Composite
- Multiple CubeSat configurations
- Pre-Qualified, assembled (Mechanical and Electrical) and ready for payload integration
- Non-Pyrotechnic Hold-Down and Release Mechanism (HDRM)
- Reconfigurable design to accommodate Hosted Payload
- Onboard Telemetry Sensors included for Deployment Confirmation and Ejection Velocity Measurement
Get a quote
Launch Solutions
Launch from PSLV / SSLV / Starship or Falcon / Vikram
Fully integrated small satellite launch solutions
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Launch from the ISS
Faster and flexible launch options
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On-orbit laboratories,
dedicated launches
dedicated launches
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MEO / GEO / Interplanetary Missions
Coming Soon
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Customised solutions
Constellation deployment services
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Assembly, integration and launch services
Launch liaising and integration services
Hosted Payloads and
standalone missions
standalone missions
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Low Earth Orbit Missions
Up to 18U payloads
Nominal lifetime: 3 years
Up to 0.1° pointing capabilities
High data rate communication FPGA-based Flight Computer
Nominal lifetime: 3 years
Up to 0.1° pointing capabilities
High data rate communication FPGA-based Flight Computer
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