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)
500 kg
Thrust
15 mN - 52 mN
DROID Comparison
DROID.alpha EP
LEO / GEO
Orbits
1.2 x 1.1 x 1.4
Size, Stowed with Payload [L x W x H]
3+ (GEO), 5+ (LEO)
Design Life (Years)
Single
Fault Tolerance
<15 arcseconds
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
Battery (Wh)
Inquire
Payload Volume [L x W x H]
1.0 x 1.0 x 1.4
Spacecraft Volume [L x W x H]
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
Communications
18 months
Current Lead Time
15 mN - 52 mN
Thrust
500 kg
Total Mass
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
Spacecraft 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
Total Mass
70 kg
Orbits
LEO / GEO
Size, stowed with payload [L x W x H]
1.2 x 1.1 x 1.4
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]
Inquire
Spacecraft Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
Current Lead Time
18 months
Thrust
40 N
Total Mass
500 kg
Orbits
LEO / GEO
Size, stowed with payload [L x W x H]
1.2 x 1.1 x 1.4
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]
Inquire
Spacecraft Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
Current Lead Time
18 months
Thrust
15 mN - 52 mN
Total Mass
500 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]
Spacecraft Volume [L x W x H]
Communications
Current Lead Time
Thrust
Total Mass
DROID.alpha EP
LEO / GEO
1.2 x 1.1 x 1.4
3+ (GEO), 5+ (LEO)
Single
<15 arcseconds
5
1,500 W
Gridded Ion Engine, Kypton
ETH, UART, PPS, 28V
2,200
Inquire
1.0 x 1.0 x 1.4
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
18 months
15 mN - 52 mN
500 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 1.4
3+ (GEO), 5+ (LEO)
Single
<10 arcseconds
5
615 W (BOL)
High purity hydrazine
ETH, UART, PPS, 28V
1,100 W
Inquire
1.0 x 1.0 x 1.4
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
18 months
40 N
500 kg
LEO / GEO
1.2 x 1.1 x 1.4
3+ (GEO), 5+ (LEO)
Single
<15 arcseconds
5
1,500 W
Gridded Ion Engine, Kypton
ETH, UART, PPS, 28V
2,200
Inquire
1.0 x 1.0 x 1.4
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
18 months
15 mN - 52 mN
500 kg
Orbits
LEO / GEO
Size, Stowed with Payload [L x W x H]
1.2 x 1.1 x 1.4
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]
Inquire
Spacecraft Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
Current Lead Time
18 months
Thrust
15 mN - 52 mN
Total Mass
500 kg
DROID.alpha EP
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
Spacecraft 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
Total Mass
70 kg
Orbits
LEO / GEO
Size, Stowed with Payload [L x W x H]
1.2 x 1.1 x 1.4
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]
Inquire
Spacecraft Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
Current Lead Time
18 months
Thrust
40 N
Total Mass
500 kg
Orbits
LEO / GEO
Size, Stowed with Payload [L x W x H]
1.2 x 1.1 x 1.4
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]
Inquire
Spacecraft Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
Current Lead Time
18 months
Thrust
15 mN - 52 mN
Total Mass
500 kg
DROID.alpha EP
LEO / GEO
Orbits
1.2 x 1.1 x 1.4
Size, Stowed with Payload [L x W x H]
3+ (GEO), 5+ (LEO)
Design Life (Years)
Single
Fault Tolerance
<15 arcseconds
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
Battery (Wh)
Inquire
Payload Volume [L x W x H]
1.0 x 1.0 x 1.4
Spacecraft Volume [L x W x H]
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
Communications
18 months
Current Lead Time
15 mN - 52 mN
Thrust
500 kg
Total Mass
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
Spacecraft 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
Total Mass
70 kg
Orbits
LEO / GEO
Size, stowed with payload [L x W x H]
1.2 x 1.1 x 1.4
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]
Inquire
Spacecraft Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
Current Lead Time
18 months
Thrust
40 N
Total Mass
500 kg
Orbits
LEO / GEO
Size, stowed with payload [L x W x H]
1.2 x 1.1 x 1.4
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]
Inquire
Spacecraft Volume [L x W x H]
1.0 x 1.0 x 1.4
Communications
S-band Tx/Rx, Ka-band Tx, L-band ISL (LEO Option)
Current Lead Time
18 months
Thrust
15 mN - 52 mN
Total Mass
500 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
