DROID.alpha Mini
Objective: Optimal for rapidly demonstrating new payloads and capabilities in space.
Options
1
Type 1 NSA Encryption or AES 256 (default)
1
Type 1 NSA Encryption or AES 256 (default)
1
Type 1 NSA Encryption or AES 256 (default)
2
Optical communications terminal (OCT) crosslink for real-time high data rate communications
2
Optical communications terminal (OCT) crosslink for real-time high data rate communications
2
Optical communications terminal (OCT) crosslink for real-time high data rate communications
3
Our payloads, your payloads, or combine.
3
Our payloads, your payloads, or combine.
3
Our payloads, your payloads, or combine.
4
Turion operated or customer operated (cloud or on-premises)
4
Turion operated or customer operated (cloud or on-premises)
4
Turion operated or customer operated (cloud or on-premises)
5
Turion handles regulatory and launch logistics
5
Turion handles regulatory and launch logistics
5
Turion handles regulatory and launch logistics
Key Specifcations
Peak power
240 W
Mass (bus only)
70 kg
Thrust
0.01 mN - 0.80 mN
DROID Comparison
DROID.alpha Mini
LEO
Orbits
0.54 x 0.51 x 0.63
Size, Stowed with Payload [L x W x H]
5+
Design Life (Years)
N/A
Fault Tolerance
<15 arcseconds
Pointing Accuracy
5
Max Slow Speed (deg/s)
240 W
Peak Power (W)
2x FEEP Thrusters
Propulsion Architecture / Fuel
ETH, UART, PPS, 28V
I/F
1,100+
Battery (Wh)
0.5 x 0.5 x 0.41
Payload Volume [L x W x H]
0.54 x 0.51 x 0.22
Bus Volume [L x W x H]
2x S, X/Ka Down
Communications
12 months
Current Lead Time
0.01 mN - 0.80 mN
Thrust
70 kg
Mass (Bus Only)
Orbits
LEO
Size, stowed with payload [L x W x H]
0.54 x 0.51 x 0.63
Design Life (Years)
5+
Fault tolerance
N/A
Pointing accuracy
<15 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
240 W
Propulsion Architecture / Fuel
2x FEEP Thrusters
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100+
Payload Volume [L x W x H]
0.5 x 0.5 x 0.41
Bus Volume [L x W x H]
0.54 x 0.51 x 0.22
Communications
2x S, X/Ka Down
Current Lead Time
12 months
Thrust
0.01 mN - 0.80 mN
Mass (Bus Only)
70 kg
Orbits
LEO / GEO
Size, stowed with payload [L x W x H]
1.2 x 1.1 x [0.8 - 1.3]
Design Life (Years)
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<10 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
615 W (BOL)
Propulsion Architecture / Fuel
High purity hydrazine
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100 W
Payload Volume [L x W x H]
1.0 x 1.0 x [0.5 - 1.0]
Bus Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
2x S Tx/Rw, Ka Down, OCT Crosslink (option)
Current Lead Time
18 months
Thrust
8 N
Mass (Bus Only)
300 kg - 400 kg
Orbits
LEO/GEO
Size, stowed with payload [L x W x H]
1.2 x 1.1 x [0.8 - 1.3]
Design Life (Years)
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<15 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
1,500 W
Propulsion Architecture / Fuel
Gridded Ion Engine, Kypton
I/F
ETH, UART, PPS, 28V
Battery (Wh)
2,200
Payload Volume [L x W x H]
1.0 x 1.0 x [0.5 - 1.0]
Bus Volume [L x W x H]
1.0 x 1.0 x [0.3 - 0.65]
Communications
2x S, Ka Downlink, OCT Crosslink (option)
Current Lead Time
12 months
Thrust
15 mN - 52 mN
Mass (Bus Only)
320 kg
Orbits
Size, Stowed with Payload [L x W x H]
Design Life (Years)
Fault Tolerance
Pointing Accuracy
Max Slew Speed (deg/s)
Peak Power (W)
Propulsion Architecture / Fuel
I/F
Battery (Wh)
Payload Volume [L x W x H]
Bus Volume [L x W x H]
Communications
Current Lead Time
Thrust
Mass (Bus Only)
DROID.alpha Mini
LEO
0.54 x 0.51 x 0.63
5+
N/A
<15 arcseconds
5
240 W
2x FEEP Thrusters
ETH, UART, PPS, 28V
1,100+
0.5 x 0.5 x 0.41
0.54 x 0.51 x 0.22
2x S, X/Ka Down
12 months
0.01 mN - 0.80 mN
70 kg
LEO
0.54 x 0.51 x 0.63
5+
N/A
<15 arcseconds
5
240 W
2x FEEP Thrusters
ETH, UART, PPS, 28V
1,100+
0.5 x 0.5 x 0.41
0.54 x 0.51 x 0.22
2x S, X/Ka Down
12 months
0.01 mN - 0.80 mN
70 kg
LEO / GEO
1.2 x 1.1 x [0.8 - 1.3]
3+ (GEO), 5+ (LEO)
Single
<10 arcseconds
5
615 W (BOL)
High purity hydrazine
ETH, UART, PPS, 28V
1,100 W
1.0 x 1.0 x [0.5 - 1.0]
1.0 x 1.0 x 1.4
2x S Tx/Rw, Ka Down, OCT Crosslink (option)
18 months
8 N
300 kg - 400 kg
LEO/GEO
1.2 x 1.1 x [0.8 - 1.3]
3+ (GEO), 5+ (LEO)
Single
<15 arcseconds
5
1,500 W
Gridded Ion Engine, Kypton
ETH, UART, PPS, 28V
2,200
1.0 x 1.0 x [0.5 - 1.0]
1.0 x 1.0 x [0.3 - 0.65]
2x S, Ka Downlink, OCT Crosslink (option)
12 months
15 mN - 52 mN
320 kg
Orbits
LEO
Size, Stowed with Payload [L x W x H]
0.54 x 0.51 x 0.63
Design Life (Years)
5+
Fault Tolerance
N/A
Pointing Accuracy
<15 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
240 W
Propulsion architecture/ fuel
2x FEEP Thrusters
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100+
Payload Volume [L x W x H]
0.5 x 0.5 x 0.41
Bus Volume [L x W x H]
0.54 x 0.51 x 0.22
Communications
2x S, X/Ka Down
Current Lead Time
12 months
Thrust
0.01 mN - 0.80 mN
Mass (Bus Only)
70 kg
DROID.alpha Mini
Orbits
LEO
Size, Stowed with Payload [L x W x H]
0.54 x 0.51 x 0.63
Design Life (Years)
5+
Fault Tolerance
N/A
Pointing Accuracy
<15 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
240 W
Propulsion architecture/ fuel
2x FEEP Thrusters
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100+
Payload Volume [L x W x H]
0.5 x 0.5 x 0.41
Bus Volume [L x W x H]
0.54 x 0.51 x 0.22
Communications
2x S, X/Ka Down
Current Lead Time
12 months
Thrust
0.01 mN - 0.80 mN
Mass (Bus Only)
70 kg
Orbits
LEO / GEO
Size, Stowed with Payload [L x W x H]
1.2 x 1.1 x [0.8 - 1.3]
Design Life (Years)
3+ (GEO), 5+ (LEO)
Fault Tolerance
Single
Pointing Accuracy
<10 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
615 W (BOL)
Propulsion architecture/ fuel
High purity hydrazine
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100 W
Payload Volume [L x W x H]
1.0 x 1.0 x [0.5 - 1.0]
Bus Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
2x S Tx/Rw, Ka Down, OCT Crosslink (option)
Current Lead Time
18 months
Thrust
8 N
Mass (Bus Only)
300 kg - 400 kg
Orbits
LEO/GEO
Size, Stowed with Payload [L x W x H]
1.2 x 1.1 x [0.8 - 1.3]
Design Life (Years)
3+ (GEO), 5+ (LEO)
Fault Tolerance
Single
Pointing Accuracy
<15 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
1,500 W
Propulsion architecture/ fuel
Gridded Ion Engine, Kypton
I/F
ETH, UART, PPS, 28V
Battery (Wh)
2,200
Payload Volume [L x W x H]
1.0 x 1.0 x [0.5 - 1.0]
Bus Volume [L x W x H]
1.0 x 1.0 x [0.3 - 0.65]
Communications
2x S, Ka Downlink, OCT Crosslink (option)
Current Lead Time
12 months
Thrust
15 mN - 52 mN
Mass (Bus Only)
320 kg
DROID.alpha Mini
LEO
Orbits
0.54 x 0.51 x 0.63
Size, Stowed with Payload [L x W x H]
5+
Design Life (Years)
N/A
Fault Tolerance
<15 arcseconds
Pointing Accuracy
5
Max Slow Speed (deg/s)
240 W
Peak Power (W)
2x FEEP Thrusters
Propulsion Architecture / Fuel
ETH, UART, PPS, 28V
I/F
1,100+
Battery (Wh)
0.5 x 0.5 x 0.41
Payload Volume [L x W x H]
0.54 x 0.51 x 0.22
Bus Volume [L x W x H]
2x S, X/Ka Down
Communications
12 months
Current Lead Time
0.01 mN - 0.80 mN
Thrust
70 kg
Mass (Bus Only)
Orbits
LEO
Size, stowed with payload [L x W x H]
0.54 x 0.51 x 0.63
Design Life (Years)
5+
Fault tolerance
N/A
Pointing accuracy
<15 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
240 W
Propulsion Architecture / Fuel
2x FEEP Thrusters
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100+
Payload Volume [L x W x H]
0.5 x 0.5 x 0.41
Bus Volume [L x W x H]
0.54 x 0.51 x 0.22
Communications
2x S, X/Ka Down
Current Lead Time
12 months
Thrust
0.01 mN - 0.80 mN
Mass (Bus Only)
70 kg
Orbits
LEO / GEO
Size, stowed with payload [L x W x H]
1.2 x 1.1 x [0.8 - 1.3]
Design Life (Years)
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<10 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
615 W (BOL)
Propulsion Architecture / Fuel
High purity hydrazine
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100 W
Payload Volume [L x W x H]
1.0 x 1.0 x [0.5 - 1.0]
Bus Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
2x S Tx/Rw, Ka Down, OCT Crosslink (option)
Current Lead Time
18 months
Thrust
8 N
Mass (Bus Only)
300 kg - 400 kg
Orbits
LEO/GEO
Size, stowed with payload [L x W x H]
1.2 x 1.1 x [0.8 - 1.3]
Design Life (Years)
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<15 arcseconds
Max Slew Speed (deg/s)
5
Peak Power (W)
1,500 W
Propulsion Architecture / Fuel
Gridded Ion Engine, Kypton
I/F
ETH, UART, PPS, 28V
Battery (Wh)
2,200
Payload Volume [L x W x H]
1.0 x 1.0 x [0.5 - 1.0]
Bus Volume [L x W x H]
1.0 x 1.0 x [0.3 - 0.65]
Communications
2x S, Ka Downlink, OCT Crosslink (option)
Current Lead Time
12 months
Thrust
15 mN - 52 mN
Mass (Bus Only)
320 kg
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Let’s Talk
Got any questions? Let’s chat and drive progress together.
Contact us
Join Us
Help us shape the future. Make an impact today.
View open positions
Let’s Talk
Got any questions? Let’s chat and drive progress together.
Contact us
Join Us
Help us shape the future. Make an impact today.
View open positions
Let’s Talk
Got any questions? Let’s chat and drive progress together.
Contact us
Join Us
Help us shape the future. Make an impact today.
View open positions
Accelerating mankind's galactic destiny
Our integrated hardware and software architecture position Turion as the foundational infrastructure for expansion into the solar system.
Resources
Accelerating mankind's galactic destiny
Our integrated hardware and software architecture position Turion as the foundational infrastructure for expansion into the solar system.
Resources
Accelerating mankind's galactic destiny
Our integrated hardware and software architecture position Turion as the foundational infrastructure for expansion into the solar system.
Resources
© 2025 Turion Space. All rights reserved. Reproduction prohibited.
© 2025 Turion Space
© 2025 Turion Space
