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Affordable Integrated GPS-Actuator GN&C System for Small Launch Vehicles, Phase I

Completed Technology Project

Project Introduction

A small launcher GNC system which maintains GPS fix while rotating, improves drift performance for COTS-based inertial sensors and provides efficient use of actuation system propellant. Provided in a package with components and systems already under development and proven in the space environment. Phase I will result in a flight test ready system More »

Anticipated Benefits

Primary U.S. Work Locations and Key Partners

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Project Management

Project Duration

Technology Maturity (TRL)

Technology Areas

Target Destination

Light bulb

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