Skip Navigation
Small Business Innovation Research/Small Business Tech Transfer

NOFBX Single-Stage-to-Orbit Mars Ascent Vehicle Engine, Phase II

Completed Technology Project

Project Introduction

NOFBX Single-Stage-to-Orbit Mars Ascent Vehicle Engine, Phase II
We propose the continuation of our research and development of a Nitrous Oxide Fuel Blend (NOFBXTM) Single-Stage-to-Orbit (SSTO) monopropellant propulsion system for future use on a Mars Ascent Vehicle (MAV) as part of the Mars Sample Return (MSR) architecture. This liquid monopropulsion system architecture is also readily scalable to alternative planetary ascent vehicles (PAV's) and sample return systems. Key areas of our proposed development and demonstration are in the nozzle miniaturization to support compact vehicle packaging into an MSR vehicle and use of a passive thrust vector control mechanism with three engines to avoid the necessity of a low temperature gimbal mechanism. More »

Primary U.S. Work Locations and Key Partners

Technology Transitions

Project Library

Share this Project

Organizational Responsibility

Project Management

Project Duration

Technology Maturity (TRL)

Technology Areas

Target Destinations

Light bulb

Suggest an Edit

Recommend changes and additions to this project record.