# Saturn-200

> spacecraft bus developed by Blue Canyon Technologies

**Wikidata**: [Q137761409](https://www.wikidata.org/wiki/Q137761409)  
**Source**: https://4ort.xyz/entity/saturn-200

## Summary
The Saturn-200 is a spacecraft bus developed by Blue Canyon Technologies, designed for minisatellites typically weighing less than 500–600 kg. It offers a payload capacity of up to 350 kg and complies with EELV Secondary Payload Adapter standards, enabling flexible integration with launch vehicles. The platform supports a range of missions, leveraging solar power and customizable configurations.

## Key Facts
- **Developer**: Blue Canyon Technologies.
- **Class**: Minisatellite (under 500–600 kg).
- **Payload Capacity**: 200 kg (standard) or 350 kg (maximum non-standard).
- **Power**: 2 spacecraft solar arrays with 1082 Wh capacity.
- **Compliance**: Meets EELV Secondary Payload Adapter standards (24 units).
- **Country of Origin**: United States.
- **Website**: https://www.bluecanyontech.com/spacecraft/saturn-200/ (English).
- **Classification**: Spacecraft model, subclass of spacecraft bus and minisatellite.

## FAQs
### Q: Who developed the Saturn-200?
A: The Saturn-200 was developed by Blue Canyon Technologies, a U.S.-based company specializing in small satellite systems.

### Q: What payload capacity does the Saturn-200 offer?
A: The Saturn-200 supports a standard payload of 200 kg and a maximum non-standard payload of 350 kg, accommodating diverse mission requirements.

### Q: What standards does the Saturn-200 comply with?
A: It complies with the EELV Secondary Payload Adapter (ESPA) standard, with compatibility for 24 units, ensuring integration with a variety of launch vehicles.

## Why It Matters
The Saturn-200 addresses the growing demand for cost-effective, adaptable small satellite platforms. Its high payload capacity (up to 350 kg) and compliance with ESPA standards make it a versatile solution for missions requiring reliable, efficient spacecraft buses. By leveraging advanced solar power systems and customizable configurations, the Saturn-200 supports a wide range of applications, from Earth observation to technology demonstration. Its design reduces development timelines and costs, democratizing access to space for commercial, academic, and government users.

## Notable For
- **High Payload Capacity**: Offers up to 350 kg for non-standard payloads, exceeding typical minisatellite limits.
- **Efficient Power System**: Features dual solar arrays with 1082 Wh capacity, optimizing energy for extended missions.
- **ESPA Compliance**: Compatible with 24-unit ESPA standards, ensuring seamless integration with EELV launch systems.
- **Customizable Design**: Supports both standard and tailored payload configurations for diverse applications.

## Body
### Overview
The Saturn-200 is a minisatellite-class spacecraft bus designed and manufactured by Blue Canyon Technologies. It serves as a modular platform for small satellite missions, emphasizing payload flexibility and compatibility with industry standards.

### Design and Specifications
- **Payload**: 
  - **Standard**: 200 kg.
  - **Maximum Non-Standard**: 350 kg.
- **Power Generation**: 
  - 2 solar arrays with a total capacity of 1082 Wh.
- **Compatibility**: 
  - Complies with EELV Secondary Payload Adapter (ESPA) standards, supporting 24-unit configurations.
- **Manufacturer**: 
  - Blue Canyon Technologies (United States).

### Technical Details
- **Class**: Minisatellite (sub-500–600 kg category).
- **Website**: https://www.bluecanyontech.com/spacecraft/saturn-200/ (English).
- **Documentation**: Specifications and performance data are detailed in the publicly available Saturn-1_2025.pdf brochure.

## References

1. [Source](https://www.bluecanyontech.com/wp-content/uploads/Saturn-1_2025.pdf)