# BCP-100

> satellite bus

**Wikidata**: [Q106457171](https://www.wikidata.org/wiki/Q106457171)  
**Source**: https://4ort.xyz/entity/bcp-100

## Summary
The BCP-100 is a spacecraft bus model designed to provide the essential infrastructure for spacecraft, serving as a service module that accommodates various payloads. It is manufactured by AeroAstro and Ball Aerospace & Technologies and is also known by alternative names including the Ball Configurable Platform 100, Astro-200, and Standard Interface Vehicle (SIV).

## Key Facts
- **Classification:** The BCP-100 is an instance of a spacecraft model and a subclass of the spacecraft bus.
- **Manufacturers:** AeroAstro and Ball Aerospace & Technologies.
- **Dimensions:** The bus measures 61 centimeters in width, 96.5 centimeters in height, and 71 centimeters in length.
- **Payload Capacity:** It supports a payload mass of at least 60 kilograms.
- **Power System:** The spacecraft is powered by a solar array capable of generating 185 watts.
- **Aliases:** Alternative designations include Ball Configurable Platform 100, Astro-200, Standard Interface Vehicle, SIV, and STP-SIV.

## FAQs
**What are the physical dimensions of the BCP-100?**
The BCP-100 spacecraft bus has a width of 61 centimeters, a height of 96.5 centimeters, and a length of 71 centimeters.

**What is the payload capacity of the BCP-100?**
The bus is designed to accommodate a payload mass that is greater than or equal to 60 kilograms.

**What power source does the BCP-100 use?**
The spacecraft model utilizes a spacecraft solar array that provides a power output of 185 watts.

**Who manufactures the BCP-100?**
The BCP-100 is manufactured by AeroAstro and Ball Aerospace & Technologies.

## Why It Matters
The BCP-100 serves as a foundational infrastructure for spacecraft, functioning as a service module that provides necessary locations for payloads such as space experiments or instruments. As a general model upon which multiple-production spacecraft can be based, it offers a standardized platform that facilitates the integration of diverse mission requirements. Its design supports the core operational needs of a spacecraft, ensuring that essential systems are in place to host and power scientific or technical instruments in space.

## Notable For
- **Standardized Interface:** Recognized as a "Standard Interface Vehicle" (SIV), facilitating easier integration of payloads.
- **Configurable Design:** Marketed as the "Ball Configurable Platform," indicating adaptability for different mission needs.
- **Dual Manufacturing:** Produced through a collaboration involving both AeroAstro and Ball Aerospace & Technologies.

## Body

### Classification and Design Role
The BCP-100 is classified as a spacecraft model and functions as a specific subclass of the broader "spacecraft bus" category. A spacecraft bus acts as the general model on which multiple-production spacecraft are often based. It constitutes the infrastructure of a spacecraft, typically providing the structural locations for the payload, which often consists of space experiments or instruments. Essentially, the BCP-100 serves as the service module section of a spacecraft, handling the critical support systems required for mission operations.

### Manufacturers
The production and development of the BCP-100 involve two primary entities: AeroAstro and Ball Aerospace & Technologies. Documentation and datasheets regarding the vehicle are archived and maintained by both organizations, reflecting their roles in its manufacturing history.

### Technical Specifications
The physical structure of the BCP-100 is defined by precise measurements. It has a width of 61 centimeters, a height of 96.5 centimeters, and a length of 71 centimeters.

In terms of capacity, the bus is engineered to support a payload mass of at least 60 kilograms. This specification allows for the accommodation of substantial experimental or instrumental hardware.

The vehicle's power system relies on a spacecraft solar array. This power source is rated for an output of 185 watts, ensuring the energy requirements of the bus and its payload are met during operation.

### Nomenclature and Documentation
The BCP-100 is known by several aliases and designations within the aerospace industry. These names include:
- Ball Configurable Platform 100
- Astro-200
- Standard Interface Vehicle (SIV)
- STP-SIV

Detailed technical descriptions of the BCP-100 are available through specific datasheets provided by the manufacturers. These documents include the "Astro 200 Series Datasheet" published by AeroAstro and the "BCP SC 3" fact sheet from Ball Aerospace & Technologies. Both documents serve as primary references for the vehicle's dimensions, power capabilities, and payload specifications.

## References

1. [Source](http://www.aeroastro.com/uploads/data%20sheets/20100004-002%20Astro%20200%20Series%20Datasheet.pdf)
2. [Source](https://www.ball.com/getattachment/bb8c3c95-42b2-4ce0-8aa7-c6f766fa0fa8/D1920_BCP_SC_3.pdf)