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Model

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100kg-class platform
150kg for payload + fuel
Price includes separation system & virtual flatsat
Bus Emulator

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The Bus Emulator includes available payload digital interfaces (Ethernet, RS422/485, LVDS, etc.), available payload power/discrete indicators, and flight-like data interface connections.

Configurations

Power

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Single-panel arrays | 215 W payload OAP
Double-panel arrays | 520 W payload OAP
Triple-panel arrays | 825 W payload OAP
SADAs

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Fixed deployable solar arrays
Single-axis SADAs for independent sun tracking
Communications

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Propulsion

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No propulsion
Monoprop
Xenon or Krypton HET
6 degree of freedom propulsion for high maneuverability
Encryption

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Default, software-based commercial encryption for bus communications
Bus support for drop-in Type 1 hardware encryption
Guidance, Navigation, and Control

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(1) Pointing knowledge: <0.02 deg 1-sigma
(2) Pointing control: <0.04 deg 1-sigma
(1) Pointing knowledge: <0.0025 deg 1-sigma
(2) Pointing control: <0.005 deg 1-sigma

Services

Payload Integration & Test

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Payload integration, functional, and environmental test according to Apex’s standard test campaign
Launch Vehicle Integration

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Spacecraft shipment to the launch site, launch site checkout, and integration with the launch vehicle
LEOP and Commissioning Service

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Mission Operations

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Model

Bus Dry Mass: 90.8 kg
Payload OAP: 215 W
View Assumptions
Total: $3,450,000
Bus Delivery: 6 months
Thank you! We will contact you very soon!
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