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Small-Scale, Methane-Fueled Reaction Control Engines for In-Space Propulsion
Completed
TRL 4 (started at 3, targeting 4)
Description
Given increasing interest in high-performance, Methane-fueled reaction control engines in the 5-100lbf thrust class, Ventions proposes the design, fabrication and hot-fire testing of a nominal 50lbf engine that is batch fabricated in a low-cost manner using a novel manufacturing process. The proposed approach leverages several years of DARPA and NASA funded work by Ventions in the successful development and ground / flight testing of such configurations, and allows for the realization of complex regenerative cooling passages and injector geometries previously unattainable by conventional fabrication methodologies.
Benefits
The 50lbf reaction control engines proposed herein can readily be scaled up or down to thrusts in the 10-250lbf range, hence, it is expected to have numerous applications for NASA missions. This is particularly true if the primary propulsion for the spacecraft is also LOX / Methane based, thereby allowing for the secondary RCE propulsion to tap off the main tankage and / or residuals. Specific examples of these applications are likely to include reaction control for human-rated spacecraft, and for lander and ascent vehicles for planetary or lunar missions (either human or large science spacecraft / rovers). Additionally, the technology is also suitable for primary ascent or descent propulsion for smaller spacecraft missions such as lunar landers, Mars hoppers, or the like thereof.
Beyond NASA missions, one can envision several non-NASA applications in the ever-growing world of commercial space. Specific examples of such commercial space missions are likely to include reaction / attitude control for large booster stages and nano launch vehicles, as well upper stage or orbit insertion propulsion. Additionally, beyond space applications, the proposed technology is also applicable in terrestrial energy markets utilizing LNG in "closed" LNG / Oxygen cycles to eliminate NOX production and simplify CO2 capture and sequestration.
Details
| Technology area | Propulsion Systems > Chemical Space Propulsion > Cryogenic Propulsion |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Astra Space, Inc, Louisville, CO |
| Start date | 2015-06-17 |
| End date | 2015-12-17 |
Project contacts
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How to get involved
This is early/mid-stage (TRL 4) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
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