650kg

PAYLOAD MASS
 

5kw

MAX SOLAR ARRAY POWER
 

1000KG

LAUNCH MASS
 

CONNECTING THE WORLD

The Enterprise builds on Terran Orbital’s long line of SmallSat bus heritage, with the same avionics and GNC algorithms as the smaller bus classes. Significant enhancements to the structure support the largest payloads, and it includes Optical Inter-Satellite Link (OISL) functionality for communications. A new power storage system has been designed to reduce weight and increase the power available to the payload.

Enterprise is scalable in thickness and weight based on customer payload requirements without changing the bus architecture. Terran Orbital employs top-of-the-line automation and modern manufacturing processes to support the delivery of hundreds of buses annually. From order to launch, in quantities from one to a constellation of one hundred, Terran Orbital accelerates the delivery of mission solutions.

KEY BENEFITS

  • Flat packing design allows delivery of up to 24 satellites per launch (depending on the launch vehicle)
  • Includes Optical Inter Satellite Link (OISL) functionality
  • Large, flat deck optimized for communications and RF payload

Baseline modules included

  • Flight Computers (2)
  • Watchdog
  • Backplane
  • 66V Battery Modules (varies)
  • 66V MPPT (10)
  • 66V Load Controller
  • 28V Low-power Point-of-Loads (varies)
  • 28V High-power Point-of-Load (varies)
  • Gyro Assembly
  • Coarse Sensors (4)
  • Star Trackers (3)
  • GPS (2)
  • Magnetorquers (3)
  • Reaction Wheels (4)
  • LDRR (2)
  • MDR (2)
  • HDR

Specifications

Configuration Flat packing
Applications LEO
Native Orbits 400km - 1200km
Launch Mass (Wet)* Up to 1000kg
Available Payload Mass 650kg
Max Solar Array Power
3rd-party solar array included
5kW
Redundancy Dual-string
Power System 66V System Power,
12V, and 9V rails available
Payload Deck Area 114.3cm x 254cm
Payload Electronics Volume 76.2cm x 30.5cm x 30.5cm
Communication Date Rate S-band: 125 Kbps uplink
2 Mbps downlink
X-band: 650 Mbps downlink
Pointing Accuracy 10 to 50 arcseconds
higher accuracy available

* maximum mass may not be supported on all launch vehicles or with all deployers.

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