Human Research Facility 1

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Human Research Facility 1 shown after its installation in the U.S. Laboratory, Destiny, during Expedition 2. - NASA Image: ISS02E6028 183436main HRF-11.jpg
Human Research Facility 1 shown after its installation in the U.S. Laboratory, Destiny, during Expedition 2. - NASA Image: ISS02E6028

Human Research Facility 1 (HRF-1) on board the International Space Station (ISS) allows investigators to study the effects of long-duration space flight on the human body. Equipment in the HRF-1 includes a clinical ultrasound and a device for measuring mass. [1]

Contents

Summary

[1]

Description

Human Research Facility 1 (HRF-1) was launched aboard STS-102 (Discovery) March 8, 2001. The HRF-1 drawers provide power, command and data handling, cooling air and water, pressurized gas, and vacuum to experiments.

The International Space Station (ISS) moderate temperature cooling loop is extended into the HRF to keep the rack at ambient temperature. The Avionics Air Assembly (AAA), which interfaces with the moderate temperature cooling loop, extracts heat from the air in the rack. Each payload can use up to 2000 W of cooling power. HRF-1 is connected to the ISS video services and Ethernet, which allow the ISS and ground operations crews to control payloads. The rack has front-panel access ports for the laptop, vacuum system, and nitrogen delivery system.

HRF-1 houses many types of equipment. Descriptions are listed below:

HRF-1 was originally launched with the following components: the ultrasound, Gas Analyzer System for Metabolic Analysis Physiology (GASMAP), portable computer, workstation, and cooling stowage drawers. During Expedition 11, the GASMAP was moved to Human Research Facility 2 (HRF-2), and SLAMMD was moved to HRF-1 from HRF-2. During Expedition 13, the original workstation was replaced with the Workstation 2. [1]

Operations

Payloads in the HRF-1 can operate independently regardless of their cooling and power needs and flight schedule. The HRF power converter delivers 120 V of direct current (DC) power from the utility outlet panel to the rack and converts it to 28 V DC for distribution to the payloads. Payload computer and video operations can be conducted from the ground or on the space station. The crew performs periodic checks of all connections and hardware and performs payload operations as needed. [1]

See also

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References

  1. 1 2 3 4 NASA.gov Human Research Facility 1 (HRF-1) - NASA

PD-icon.svg This article incorporates  public domain material from the NASA document: "Human Research Facility 1 (HRF-1)".