Launch
solutions

Enabling rapid satellite deployment for multiple platform sizes and from various launch vehicle providers.

Discover
Discover
Fully Customisable
Fully Customisable
Faster Lead Time
Rapid Constellation Deployment
Non Pyro technic HDRM
Non-Pyrotechnic HDRM
Side volume for solar panels
Side Volume for Solar Panels
1-32Kgs Payload
1 to 32 kg Payload
Upto 16U volume available
Upto 16U Volume Available
Make in India
Make In India
Dhruva Space

satellite Orbital
Deployers
range

DSOD 1UDhruva Space
1U
Orbital Deployer
DSOD 3UDhruva Space
3U
Orbital Deployer
DSOD 6UDhruva Space
6U
Orbital Deployer
DSOD 12UDhruva Space
12U
Orbital Deployer
DSOD 16UDhruva Space
16U
Orbital Deployer

DSOD 1U

Dhruva Space Satellite Orbital Deployer 1U
DSOD 1U
CubeSat Form Factor
1U, 2 x 0.5U etc
Total CubeSat Mass
2 kg
Side
Volume
Upto 9 mm on all sides
Ejection Velocity
< 2 m/s
  • Multiple CubeSat configurations
  • Space-qualified, Pre-qualified, assembled (mechanical, 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
Request Interface Control Document

DSOD 3U

Dhruva Space Satellite Orbital Deployer 3U
DSOD 3U
CubeSat Form Factor
1U, 1.5U, 2U, 3U
Total CubeSat Mass
6 kg
Side
Volume
Upto 9 mm on all sides
Ejection Velocity
< 2 m/s
  • Multiple CubeSat configurations
  • Pre-qualified and assembled (Mechanical, Electrical) & 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.
Request Interface Control Document

DSOD 12U

Dhruva Space Satellite Orbital Deployer 12U
DSOD 12U
CubeSat
form factor
1U, 1.5U, 2U, 3U, 6U, 12U
Total CubeSat mass
24 kg
Side
Volume
Upto 9 mm on all sides
Ejection Velocity
< 2 m/s
  • Multiple CubeSat configurations
  • Pre-qualified and assembled (Mechanical, Electrical) & 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.
Request Interface Control Document

DSOD 16U

Dhruva Space Satellite Orbital Deployer 16U
DSOD 16U
CubeSat
form factor
1U, 1.5U, 2U, 3U, 6U, 12U
Total CubeSat mass
32 kg
Side
Volume
Upto 9 mm on all sides
Ejection Velocity
< 2 m/s
  • Multiple CubeSat configurations
  • Pre-qualified and assembled (Mechanical, Electrical) & 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.
Request Interface Control Document

DSOD 6U

Dhruva Space Satellite Orbital Deployer 6U
DSOD 1U
CubeSat Form Factor
1U, 2 x 0.5U etc
Total CubeSat Mass
2 kg
Side
Volume
Upto 9 mm on all sides
Ejection Velocity
< 2 m/s
  • Multiple CubeSat configurations
  • Space-qualified, Pre-qualified, assembled (mechanical, 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
Request Interface Control Document

Hosted
Payloads

Select a unique space service for your payload, including advanced features such as:
Space Cloud, and Virtual Machine Applications

Launch from International Space Station

Launch from International Space Station
  • Upto 10U Payloads
  • Flight computer with power and communication
  • Return to Earth at end of mission
  • Upto 3 months in orbit
  • Microgravity experiments
  • Technology demonstrations
  • Material Sciences | Fluid Sciences | Biological Sciences
Launch from InternationalSpace Station
Dhruva Space

Payload Parameters

Average power available
5-30 W
Peak power available
50 W
Power buses available
6-12 V
Customizable
Additional custom buses
24 V
36 V upon request
Maximum payload mass
7 kg
Request user guide
Dhruva Space

Book Your Mission

Set your payload
requirements
Select your
mission
Get to
orbit
Time until next launch
Book Now

Launch
solutions

Launch from
PSLV / Starship or Falcon / Vikram
Fully integrated small satellite launch solutions
Launch from the
ISS
Faster, flexible launch options
On-orbit laboratories, dedicated launches
Customized solutions for critical payload  requirements / Falcon / Vikram
Constellation deployment services
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
Assembly, integration and launch services 
Integration facilities and testing support
Hosted payloads, standalone missions
MEO/GEO/INTERPLANETARY MISSIONS
Coming soon

Get detailed specs

Thank you! Your submission has been received!
Oops! Something went wrong while submitting the form.
Dhruva Space

Request for Information

Thank you! Your submission has been received!
Oops! Something went wrong while submitting the form.
X