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Legacy EO-1 Site
Introduction
Go to Legacy EO-1 Site

Baseline Mission
Introduction

Spacecraft Bus
Introduction

Technology Validation
Introduction
Instrument Technology Overview
Instrument Validation Summaries & Reports
Spacecraft Bus Technology Overview
Spacecraft Bus Validation Summaries & Reports

Science Validation
Introduction
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Lessons Learned
Introduction

Continuous Improvement
Introduction
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Launch
Introduction
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Education
Outreach



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Technology Validation  
Spacecraft Bus Technology Overview

Related

READ MORE >>
Read and download the full EO-1 Validation Report.

Related Sites
USGS/EO-1 website at
http://eo1.usgs.gov

Contact
Questions and comments related to this document should be directed to:

Joseph Young
EO-1 Technology Transfer Manager
EO-1 Mission Office
NASA Goddard Space Flight Center
Greenbelt, MD 20771
Phone: 301-286-8146
Fax: 301-286-1736
E-Mail: Joe Young

The following spacecraft bus crosscutting technologies, which will reduce the cost, mass and complexity of future Earth observing spacecraft and allow more scientific payload to fly on future missions, were demonstrated by EO-1:

X-Band Phased Array Antenna

Wideband Advanced Recorder / Processor

Enhanced Formation Flying

Pulsed Plasma Thruster

Lightweight Flexible Solar Array

Carbon-Carbon Radiator

LA-II Thermal Coating

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