DROID.alpha EP
Objective: Optimal platform for higher delta-V solutions like vLEO remote sensing, ISAM, and Cislunar applications.
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
1,500 W
Mass (bus only)
320 kg
Thrust
15-52 mN
DROID Comparison
DROID.alpha EP
LEO/GEO
Orbits
1.2 x 1.1 x [0.8-1.3]
Size, stowed with payload [L x W x H]
3+ (GEO), 5+ (LEO)
Design life
Single
Fault tolerance
<15 arcsecond
Pointing accuracy
5
Max slow speed (deg/s)
1,500 W
Peak power (W)
Gridded Ion Engine, Kypton
Propulsion architecture / fuel
ETH, UART, PPS, 28V
I/F
2,200 W-hours
Battery (Wh)
1.0 x 1.0 x [0.5-1.0]
Payload volume [L x W x H]
1.0 x 1.0 x [0.3-0.65]
Bus volume [L x W x H]
2x S, Ka Down, OCT Crosslink (option)
Comms
12 months
Current lead time
15-52 mN
Thrust
320 kg
Mass (bus only)
Orbits
LEO
Size, stowed with payload [L x W x H]
0.54 x 0.51 x 063
Design life
5+
Fault tolerance
N/A
Pointing accuracy
<15 arcsecond
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
Comms
2x S, X/Ka Down
Current lead time
12 months
Thrust
.01-.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
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<10 arcseond
Max slew speed (deg/s)
5
Peak power (W)
400 W
Propulsion architecture / fuel
Hydrazine thrusters, 6DoF dual-string
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100 W-hours
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]
Comms
2x S, Ka Down, OCT Crosslink (option)
Current lead time
12 months
Thrust
8 N
Mass (bus only)
350 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
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<15 arcsecond
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 W-hours
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]
Comms
2x S, Ka Down, OCT Crosslink (option)
Current lead time
12 months
Thrust
15-52 mN
Mass (bus only)
320 kg
Orbits
Size, stowed with payload [L x W x H]
Design life
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]
Comms
Current lead time
Thrust
Mass (bus only)
DROID.alpha EP
LEO/GEO
1.2 x 1.1 x [0.8-1.3]
3+ (GEO), 5+ (LEO)
Single
<15 arcsecond
5
1,500 W
Gridded Ion Engine, Kypton
ETH, UART, PPS, 28V
2,200 W-hours
Gridded Ion Engine, Kypton
1.0 x 1.0 x [0.3-0.65]
2x S, Ka Down, OCT Crosslink (option)
12 months
15-52 mN
320 kg
LEO
0.54 x 0.51 x 063
5+
N/A
<15 arcsecond
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
.01-.80 mN
70 kg
LEO/GEO
1.2 x 1.1 x [0.8-1.3]
3+ (GEO), 5+ (LEO)
Single
<10 arcseond
5
400 W
Hydrazine thrusters, 6DoF dual-string
ETH, UART, PPS, 28V
1,100 W-hours
1.0 x 1.0 x [0.5-1.0]
1.0 x 1.0 x [0.3-0.65]
2x S, Ka Down, OCT Crosslink (option)
12 months
8 N
350 kg
LEO/GEO
1.2 x 1.1 x [0.8-1.3]
3+ (GEO), 5+ (LEO)
Single
<15 arcsecond
5
1,500 W
Gridded Ion Engine, Kypton
ETH, UART, PPS, 28V
2,200 W-hours
1.0 x 1.0 x [0.5-1.0]
1.0 x 1.0 x [0.3-0.65]
2x S, Ka Down, OCT Crosslink (option)
12 months
15-52 mN
320 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
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<15 arcsecond
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 W-hours
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]
Comms
2x S, Ka Down, OCT Crosslink (option)
Current lead time
12 months
Thrust
15-52 mN
Mass (bus only)
320 kg
DROID.alpha EP
Orbits
LEO
Size, stowed with payload [L x W x H]
0.54 x 0.51 x 063
Design life
5+
Fault tolerance
N/A
Pointing accuracy
<15 arcsecond
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
Comms
2x S, X/Ka Down
Current lead time
12 months
Thrust
.01-.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
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<10 arcseond
Max slew speed (deg/s)
5
Peak power (W)
400 W
Propulsion architecture/ fuel
Hydrazine thrusters, 6DoF dual-string
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100 W-hours
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]
Comms
2x S, Ka Down, OCT Crosslink (option)
Current lead time
12 months
Thrust
8 N
Mass (bus only)
350 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
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<15 arcsecond
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 W-hours
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]
Comms
2x S, Ka Down, OCT Crosslink (option)
Current lead time
12 months
Thrust
15-52 mN
Mass (bus only)
320 kg
DROID.alpha EP
LEO/GEO
Orbits
1.2 x 1.1 x [0.8-1.3]
Size, stowed with payload [L x W x H]
3+ (GEO), 5+ (LEO)
Design life
Single
Fault tolerance
<15 arcsecond
Pointing accuracy
5
Max slow speed (deg/s)
1,500 W
Peak power (W)
Gridded Ion Engine, Kypton
Propulsion architecture / fuel
ETH, UART, PPS, 28V
I/F
2,200 W-hours
Battery (Wh)
1.0 x 1.0 x [0.5-1.0]
Payload volume [L x W x H]
1.0 x 1.0 x [0.3-0.65]
Bus volume [L x W x H]
2x S, Ka Down, OCT Crosslink (option)
Comms
12 months
Current lead time
15-52 mN
Thrust
320 kg
Mass (bus only)
Orbits
LEO
Size, stowed with payload [L x W x H]
0.54 x 0.51 x 063
Design life
5+
Fault tolerance
N/A
Pointing accuracy
<15 arcsecond
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
Comms
2x S, X/Ka Down
Current lead time
12 months
Thrust
.01-.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
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<10 arcseond
Max slew speed (deg/s)
5
Peak power (W)
400 W
Propulsion architecture / fuel
Hydrazine thrusters, 6DoF dual-string
I/F
ETH, UART, PPS, 28V
Battery (Wh)
1,100 W-hours
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]
Comms
2x S, Ka Down, OCT Crosslink (option)
Current lead time
12 months
Thrust
8 N
Mass (bus only)
350 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
3+ (GEO), 5+ (LEO)
Fault tolerance
Single
Pointing accuracy
<15 arcsecond
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 W-hours
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]
Comms
2x S, Ka Down, OCT Crosslink (option)
Current lead time
12 months
Thrust
15-52 mN
Mass (bus only)
320 kg
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Let’s Talk
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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.
Products
Resources
Accelerating mankind's galactic destiny
Our integrated hardware and software architecture position Turion as the foundational infrastructure for expansion into the solar system.
Products
Resources
Accelerating mankind's galactic destiny
Our integrated hardware and software architecture position Turion as the foundational infrastructure for expansion into the solar system.
Products
Resources
© 2025 Turion Space. All rights reserved. Reproduction prohibited.
© 2025 Turion Space
© 2025 Turion Space
