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Model

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Model: Aries
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
Quad-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
High maneuverability, up to 800 m/s delta-v
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

Coming Soon

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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Close button
Reserve Your Bus
Continue to reserveration
Close button
Model: GEO Aries
175kg-class platform
120kg for payload + fuel
Price includes separation system & virtual flatsat

Configurations

Power

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Double-panel arrays | 115W payload OAP
Double-panel arrays | 520 W payload OAP
Quad-panel arrays | 825 W payload OAP
SADAs

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Single-axis SADAs for independent sun tracking
Single-axis SADAs for independent sun tracking
Communications

Select one

Propulsion

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High maneuverability, up to 800 m/s delta-v
Choice of efficiency and maneuverability
Xenon or Krypton HET
6 degree of freedom propulsion for high maneuverability
Encryption

Select one

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

Select one

<0.0025° pointing knowledge 1-sigma
<0.005° pointing accuracy 1-sigma
(1) Pointing knowledge: <0.0025 deg 1-sigma
(2) Pointing control: <0.005 deg 1-sigma

Services

Payload Integration & Test

Check box to include

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

Check box to include

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

Coming Soon

Mission Operations

Coming Soon

Model

Bus Dry Mass: 90.8 kg
Payload OAP: 115 W
View Assumptions
Total: $13,500,000
Bus Delivery: 20 months
Thank you! We will contact you very soon!
Oops! Something went wrong while submitting the form.
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