Product & Solutions

COMMUNICATIONS & NETWORKING SOLUTIONS
CYBER SECURITY SOLUTIONS
PROCESSING & PAYLOAD INTERFACE ELECTRONICS SOLUTIONS
BUS & PAYLOAD INTEGRATED AVIONICS SOLUTIONS

SCR-104

Overview:

S-Band Software-defined Compact Radio (SCR)

On-Orbit Configurable
USB and AFSCN SGLS Support
Ranging Support (PN/PRN)

Key Characteristics:

Uplink Frequency Bands: L-Band/S-Band

Downlink Frequency Band: S-Band

RF Power: Up to 2 W

Downlink Data Rate: 4.5+ Mbps

Modulation: BPSK, QPSK, OQPSK

Options:

AES-256 Encryption
Diplexer/Splitter
High Power Amplifier (HPA)

Size, Weight & Power:

Size (excluding diplexer/splitter):

CubeSat: 82 x 82 x 25 mm
SmallSat: 98 x 82 x 33 mm

Mass:

CubeSat: 250 g
SmallSat: 290 g

Power:

3-15 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2019

SCR-106 / SCR-106HDR

Overview:

X-Band Software-defined Compact Radio (SCR)

On-Orbit Configurable
AFSCN SGLS & Non-SGLS Support
Ranging Support (PN/PRN)

Key Characteristics:

Uplink Frequency Bands: L-Band/S-Band

Downlink Frequency Band: X-Band

RF Power: Up to 2 W

Downlink Data Rate:

Up to 20 Mbps (SCR-106)
Up to 100 Mbps (SCR-106HDR)

Modulation: BPSK, QPSK, OQPSK

Options:

AES-256 Encryption
High Power Amplifier (HPA)
X-Band Uplink

Size, Weight & Power:

Form Factor: CubeSat or SmallSat

Size:

CubeSat: 82 x 82 x 25 mm
SmallSat: 98 x 82 x 28 mm

Mass:

CubeSat: 250 g
SmallSat: 290 g

Power:

3.5-30 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2022

SCR-108

Overview:

Ka-Band Software-defined Compact Radio (SCR)

On-Orbit Configurable
Ranging Support (PN/PRN)

Key Characteristics:

Uplink Frequency Band: Ka-Band

Downlink Frequency Band: Ka-Band

RF Power: Up to 3 W

Data Rate: Up to 100 Mbps

Modulation: BPSK, QPSK, OQPSK, 8PSK

Options:

AES-256 Encryption
High Power Amplifier (HPA)

Size, Weight & Power:

Form Factor: SmallSat

Size:

98 x 87 x 39 mm

Mass:

404 g

Power:

12-50 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 7

Flight Heritage: Expected in 2023

RTR-400XS

Overview:

Networking Internet Protocol (IP) Router (RTR)

Based on CFC-400XS Hardware Platform
On-Orbit Re-Programmable

Key Characteristics:

Open Systems Interconnection (OSI) Layer 3 IP/MPLS Router

Supports Up to 8x 100/1000 Base-T (GbE) Ethernet Ports

Interfaces: 8x 100/1000 Base-T (GbE) Ethernet Ports

Processing: Defense-Grade Xilinx UltraScale+ Multi-Processor System-on-Chip (MPSoC)

Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: CubeSat

Size:

82 x 82 x 43 mm

Mass:

310 g

Power:

20 W Max

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2023

SWC-400XS

Overview:

Networking Ethernet Switch (SWC)

Based on CFC-400XS Hardware Platform
On-Orbit Re-Programmable

Key Characteristics:

Open Systems Interconnection (OSI) Layer 2 Ethernet Switch

Interfaces: 8x 100/1000 Base-T (GbE) Ethernet Ports

Processing: Defense-Grade Xilinx UltraScale+ Multi-Processor System-on-Chip (MPSoC)

Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: CubeSat

Size:

82 x 82 x 43 mm

Mass:

310 g

Power:

20 W Max

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2023

KI-103 (a.k.a. Gnome)

Overview:

“Bulk” End Cryptographic Unit (ECU)

Top Secret and Below (TSAB) Certified
Ideal for Telemetry, Tracking & Command (TT&C) Link and Mission Data Link (MDL)
Re-Programmable Keys for ease of Assembly, Integration and Test (AI&T)

Key Characteristics:

Data Rate: Up to 40 Mbps

Over-the-Air Rekey (OTAR) Support

Integrated with Innoflight’s SCRs (SCR-104, SCR-106, SCR-106HDR, and SCR-108) for Compact Secure Communications

Size, Weight & Power:

Form Factor: CubeSat

Size:

83 x 84 x 15 mm

Mass:

165 g

Power:

2.0 W Max / 0.9 W Low-Power Mode

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2019

CFC-400XS

Overview:

General Purpose Processor (GPP) Compact Flight Computer (CFC)

High Performance
Based on Legacy CFC-400 Hardware Platform
On-Orbit Re-Programmable
Ideal for Command and Data Handling (C&DH), Payload Interface & Data Processing, and Battle Management Command, Control and Communications (BMC3) Applications

Key Characteristics:

Processing: Defense-Grade Xilinx UltraScale+ Multi-Processor System-on-Chip (MPSoC)

Processor System-on-Chip (MPSoC)
Variety of Daughter Cards with Interfaces:

Low + Medium + High Speed Serial
3x-8x 1000 Base-T (GbE) Ethernet

Includes Linux Reference Design
Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: CubeSat

Size:

82 x 82 x 43 mm

Mass:

350 g

Power:

6-25 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2021

CFC-405XP / CFC-450XP

Overview:

General Purpose Processor (GPP) Compact Flight Computer (CFC)

High Performance
Based on the Legacy CFC-400XS Hardware Platform
On-Orbit Re-Programmable
Ideal for Command and Data Handling (C&DH), Payload Interface & Data Processing, and Battle Management Command, Control and Communications (BMC3) Applications

Key Characteristics:

Processing: Defense-Grade Xilinx UltraScale+ Multi-Processor System-on-Chip (MPSoC)

Variety of Serial and Ethernet Interfaces

Includes Linux Reference Design

Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: 3U-VPX Module

Size:

172 x 100 x 25 mm

Mass:

610 g

Power:

4-30 W

Technology Readiness Level (TRL) & Flight Heritage:

TRLs:

9 (CFC-400XS)
5 (CFC-400XP)

Flight Heritage:

CFC-400XS: Since 2021
CFC-400XP: Expected in 2024

CFC-510P

Overview:

Graphics Processing Unit (GPU) Compact Flight Computer (CFC)

High Performance
Based on Legacy CFC-500S/CFC-500P (NVIDIA Tegra K1 GPU) Hardware Platform
On-Orbit Re-Programmable
Ideal for Command and Data Handling (C&DH), Payload Interface & Data Processing, and Battle Management Command, Control and Communications (BMC3) Applications

Key Characteristics:

Processing: AMD Ryzen GPU

Includes Linux Reference Design + CUDA Runtime Environment

Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: 3U-VPX Module

Size:

172 x 100 x 25 mm

Mass:

610 g

Power:

5-30 W

Technology Readiness Level (TRL) & Flight Heritage:

TRLs:

7 (CFC-500P)
5 (CFC-510P)

Flight Heritage:

CFC-500P: Expected in 2023
CFC-510P: Expected in 2024

SSD-2000

Overview:

Solid-State Drive (SSD)

Up to 2 TB of storage

Key Characteristics:

2x PCIe m.2 SSDs

Read – 1,300 MB/s
Write – 500 MB/s

I/O through VPX Backplane

Encryption at Rest

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: 3U-VPX Module

Size:

172 x 100 x 25 mm

Mass:

Power:

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 5

Flight Heritage: Expected in 2024

IOI-8

Overview:

Input/Output Interfaces (IOI)

Variety of I/O Interfaces including Ethernet

Key Characteristics:

Interfaces:

4x 10GBase-T (10 GbE)
4x 1000Base-T (GbE)

Size, Weight & Power:

Form Factor: 3U-VPX Module

Size:

172 x 100 x 25 mm

Mass:

Power:

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 5

Flight Heritage: Expected in 2024

MTE-110

Overview:

High Precision Mission Timing Electronics (MTE)

High accuracy timing operations for spacecraft bus or mission payload

Key Characteristics:

Inputs: 2x PPS

Outputs:

12x+ PPS
8x 10 MHz

Embedded Chip Scale Atomic Clock (CSAC)
Radiation Tolerant Design

Size, Weight & Power:

Form Factor: CubeSat

Size:

82 x 82 x 38 mm

Mass:

250 g

Power:

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2023

MNE-405 / MNE-410

Overview:

Mission Networking Electronics (MNE)

3U-VPX Chassis
Internet Protocol (IP) Router (RTR), Ethernet Switch (SWC) or MPLS Router (SNP: Secure Network Processor: SNP) Personalities

Key Characteristics:

2-Slot 3U-VPX Chassis:

1x CFC-400XP (MNE-400) or 1x CFC-405XP (MNE-405) or 1x CFC-450XP (MNE-410) Module (4x 1000Base-T)
1x IOI-8 Module (4x 10GBase-T + 4x 1000Base-T)

Size, Weight & Power:

Form Factor: 3U-VPX Chassis

Size:

197 x 150 x 82 mm

Mass:

2.7 kg

Power:

40 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 5

Flight Heritage: Expected in 2024

MPE-405 / MPE-410 / MPE-605 / MPE-610

Overview:

Mission Processing Electronics (MPE)

3U-VPX Chassis
Ideal for Command and Data Handling (C&DH), Payload Interface & Data Processing, and Battle Management Command, Control and Communications (BMC3) Applications

Key Characteristics:

2-Slot (MPE-405) or 4-Slot (MPE-605) 3U-VPX Chassis

3U-VPX Compatible Modules:

CFC-400XP (Controller or Processing)
CFC-510P (Processing)
SSD-2000 (Storage)
IOI-8 (Interfaces)

Size, Weight & Power:

Form Factor: 3U-VPX Chassis

Size:

197 x 151 x 83 mm (MPE-405)
201 x 176 x 111 mm (MPE-605)

Mass:

2.7 Kg (MPE-405)
4.7 kg (MPE-605)

Power:

60 W Max (MPE-405)
100 W Max (MPE-605)

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 5

Flight Heritage: Expected in 2024

SCR-104

Overview:

S-Band Software-defined Compact Radio (SCR)

On-Orbit Configurable
USB and AFSCN SGLS Support
Ranging Support (PN/PRN)

Key Characteristics:

Uplink Frequency Bands: L-Band/S-Band

Downlink Frequency Band: S-Band

RF Power: Up to 2 W

Downlink Data Rate: 4.5+ Mbps

Modulation: BPSK, QPSK, OQPSK

Options:

AES-256 Encryption
Diplexer/Splitter
High Power Amplifier (HPA)

Size, Weight & Power:

Size (excluding diplexer/splitter):

CubeSat: 82 x 82 x 25 mm
SmallSat: 98 x 82 x 33 mm

Mass:

CubeSat: 250 g
SmallSat: 290 g

Power:

3-15 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2019

SCR-106 / SCR-106HDR

Overview:

X-Band Software-defined Compact Radio (SCR)

On-Orbit Configurable
AFSCN SGLS & Non-SGLS Support
Ranging Support (PN/PRN)

Key Characteristics:

Uplink Frequency Bands: L-Band/S-Band

Downlink Frequency Band: X-Band

RF Power: Up to 2 W

Downlink Data Rate:

Up to 20 Mbps (SCR-106)
Up to 100 Mbps (SCR-106HDR)

Modulation: BPSK, QPSK, OQPSK

Options:

AES-256 Encryption
High Power Amplifier (HPA)
X-Band Uplink

Size, Weight & Power:

Form Factor: CubeSat or SmallSat

Size:

CubeSat: 82 x 82 x 25 mm
SmallSat: 98 x 82 x 28 mm

Mass:

CubeSat: 250 g
SmallSat: 290 g

Power:

3.5-30 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2022

SCR-108

Overview:

Ka-Band Software-defined Compact Radio (SCR)

On-Orbit Configurable
Ranging Support (PN/PRN)

Key Characteristics:

Uplink Frequency Band: Ka-Band

Downlink Frequency Band: Ka-Band

RF Power: Up to 3 W

Data Rate: Up to 100 Mbps

Modulation: BPSK, QPSK, OQPSK, 8PSK

Options:

AES-256 Encryption
High Power Amplifier (HPA)

Size, Weight & Power:

Form Factor: SmallSat

Size:

98 x 87 x 39 mm

Mass:

404 g

Power:

12-50 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 7

Flight Heritage: Expected in 2023

RTR-400XS

Overview:

Networking Internet Protocol (IP) Router (RTR)

Based on CFC-400XS Hardware Platform
On-Orbit Re-Programmable

Key Characteristics:

Open Systems Interconnection (OSI) Layer 3 IP/MPLS Router

Supports Up to 8x 100/1000 Base-T (GbE) Ethernet Ports

Interfaces: 8x 100/1000 Base-T (GbE) Ethernet Ports

Processing: Defense-Grade Xilinx UltraScale+ Multi-Processor System-on-Chip (MPSoC)

Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: CubeSat

Size:

82 x 82 x 43 mm

Mass:

310 g

Power:

20 W Max

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2023

SWC-400XS

Overview:

Networking Ethernet Switch (SWC)

Based on CFC-400XS Hardware Platform
On-Orbit Re-Programmable

Key Characteristics:

Open Systems Interconnection (OSI) Layer 2 Ethernet Switch

Interfaces: 8x 100/1000 Base-T (GbE) Ethernet Ports

Processing: Defense-Grade Xilinx UltraScale+ Multi-Processor System-on-Chip (MPSoC)

Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: CubeSat

Size:

82 x 82 x 43 mm

Mass:

310 g

Power:

20 W Max

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2023

KI-103 (a.k.a. Gnome)

Overview:

“Bulk” End Cryptographic Unit (ECU)

Top Secret and Below (TSAB) Certified
Ideal for Telemetry, Tracking & Command (TT&C) Link and Mission Data Link (MDL)
Re-Programmable Keys for ease of Assembly, Integration and Test (AI&T)

Key Characteristics:

Data Rate: Up to 40 Mbps

Over-the-Air Rekey (OTAR) Support

Integrated with Innoflight’s SCRs (SCR-104, SCR-106, SCR-106HDR, and SCR-108) for Compact Secure Communications

Size, Weight & Power:

Form Factor: CubeSat

Size:

83 x 84 x 15 mm

Mass:

165 g

Power:

2.0 W Max / 0.9 W Low-Power Mode

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2019

CFC-400XS

Overview:

General Purpose Processor (GPP) Compact Flight Computer (CFC)

High Performance
Based on Legacy CFC-400 Hardware Platform
On-Orbit Re-Programmable
Ideal for Command and Data Handling (C&DH), Payload Interface & Data Processing, and Battle Management Command, Control and Communications (BMC3) Applications

Key Characteristics:

Processing: Defense-Grade Xilinx UltraScale+ Multi-Processor System-on-Chip (MPSoC)

Processor System-on-Chip (MPSoC)
Variety of Daughter Cards with Interfaces:

Low + Medium + High Speed Serial
3x-8x 1000 Base-T (GbE) Ethernet

Includes Linux Reference Design
Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: CubeSat

Size:

82 x 82 x 43 mm

Mass:

350 g

Power:

6-25 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2021

CFC-405XP / CFC-450XP

Overview:

General Purpose Processor (GPP) Compact Flight Computer (CFC)

High Performance
Based on the Legacy CFC-400XS Hardware Platform
On-Orbit Re-Programmable
Ideal for Command and Data Handling (C&DH), Payload Interface & Data Processing, and Battle Management Command, Control and Communications (BMC3) Applications

Key Characteristics:

Processing: Defense-Grade Xilinx UltraScale+ Multi-Processor System-on-Chip (MPSoC)

Variety of Serial and Ethernet Interfaces

Includes Linux Reference Design

Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: 3U-VPX Module

Size:

172 x 100 x 25 mm

Mass:

610 g

Power:

4-30 W

Technology Readiness Level (TRL) & Flight Heritage:

TRLs:

9 (CFC-400XS)
5 (CFC-400XP)

Flight Heritage:

CFC-400XS: Since 2021
CFC-400XP: Expected in 2024

CFC-510P

Overview:

Graphics Processing Unit (GPU) Compact Flight Computer (CFC)

High Performance
Based on Legacy CFC-500S/CFC-500P (NVIDIA Tegra K1 GPU) Hardware Platform
On-Orbit Re-Programmable
Ideal for Command and Data Handling (C&DH), Payload Interface & Data Processing, and Battle Management Command, Control and Communications (BMC3) Applications

Key Characteristics:

Processing: AMD Ryzen GPU

Includes Linux Reference Design + CUDA Runtime Environment

Radiation Tolerant Supervisor

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: 3U-VPX Module

Size:

172 x 100 x 25 mm

Mass:

610 g

Power:

5-30 W

Technology Readiness Level (TRL) & Flight Heritage:

TRLs:

7 (CFC-500P)
5 (CFC-510P)

Flight Heritage:

CFC-500P: Expected in 2023
CFC-510P: Expected in 2024

SSD-2000

Overview:

Solid-State Drive (SSD)

Up to 2 TB of storage

Key Characteristics:

2x PCIe m.2 SSDs

Read – 1,300 MB/s
Write – 500 MB/s

I/O through VPX Backplane

Encryption at Rest

Includes CyberDog™ Software Suite

Size, Weight & Power:

Form Factor: 3U-VPX Module

Size:

172 x 100 x 25 mm

Mass:

Power:

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 5

Flight Heritage: Expected in 2024

IOI-8

Overview:

Input/Output Interfaces (IOI)

Variety of I/O Interfaces including Ethernet

Key Characteristics:

Interfaces:

4x 10GBase-T (10 GbE)
4x 1000Base-T (GbE)

Size, Weight & Power:

Form Factor: 3U-VPX Module

Size:

172 x 100 x 25 mm

Mass:

Power:

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 5

Flight Heritage: Expected in 2024

MTE-110

Overview:

High Precision Mission Timing Electronics (MTE)

High accuracy timing operations for spacecraft bus or mission payload

Key Characteristics:

Inputs: 2x PPS

Outputs:

12x+ PPS
8x 10 MHz

Embedded Chip Scale Atomic Clock (CSAC)
Radiation Tolerant Design

Size, Weight & Power:

Form Factor: CubeSat

Size:

82 x 82 x 38 mm

Mass:

250 g

Power:

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 9

Flight Heritage: Since 2023

MNE-405 / MNE-410

Overview:

Mission Networking Electronics (MNE)

3U-VPX Chassis
Internet Protocol (IP) Router (RTR), Ethernet Switch (SWC) or MPLS Router (SNP: Secure Network Processor: SNP) Personalities

Key Characteristics:

2-Slot 3U-VPX Chassis:

1x CFC-400XP (MNE-400) or 1x CFC-405XP (MNE-405) or 1x CFC-450XP (MNE-410) Module (4x 1000Base-T)
1x IOI-8 Module (4x 10GBase-T + 4x 1000Base-T)

Size, Weight & Power:

Form Factor: 3U-VPX Chassis

Size:

197 x 150 x 82 mm

Mass:

2.7 kg

Power:

40 W

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 5

Flight Heritage: Expected in 2024

MPE-405 / MPE-410 / MPE-605 / MPE-610

Overview:

Mission Processing Electronics (MPE)

3U-VPX Chassis
Ideal for Command and Data Handling (C&DH), Payload Interface & Data Processing, and Battle Management Command, Control and Communications (BMC3) Applications

Key Characteristics:

2-Slot (MPE-405) or 4-Slot (MPE-605) 3U-VPX Chassis

3U-VPX Compatible Modules:

CFC-400XP (Controller or Processing)
CFC-510P (Processing)
SSD-2000 (Storage)
IOI-8 (Interfaces)

Size, Weight & Power:

Form Factor: 3U-VPX Chassis

Size:

197 x 151 x 83 mm (MPE-405)
201 x 176 x 111 mm (MPE-605)

Mass:

2.7 Kg (MPE-405)
4.7 kg (MPE-605)

Power:

60 W Max (MPE-405)
100 W Max (MPE-605)

Technology Readiness Level (TRL) & Flight Heritage:

TRL: 5

Flight Heritage: Expected in 2024

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