TR-107

{{Short description|Proposed US kerolox rocket engine}}

{{infobox rocket engine

| name = TR-107

| image = TR107 Prototype Engine.png

| country_of_origin = United States

| manufacturer = Northrop Grumman

| purpose = low cost throttleable booster engine

| type = liquid

| fuel = RP-1 (kerosene)

| oxidiser = LOX

| thrust(SL) = {{convert|4900|kN|lbf|abbr=on}}

| thrust(Vac) =

| specific_impulse_vacuum =

| specific_impulse_sea_level =

| chamber_pressure = 177 bar

| thrust_to_weight =

| cycle =

| diameter =

| height =

| dry_weight = {{convert|00|kg|abbr=on}}

}}

The TR-107 was a developmental rocket engine designed in 2002 by Northrop Grumman for the NASA and DoD-funded Space Launch Initiative (SLI). Operating on LOX/RP-1, the engine was throttleable and had a thrust of {{convert|4900|kN|lbf|abbr=on}} at a chamber pressure of {{convert|177|bar|MPa|disp=flip}}, making it one of the most powerful engines ever constructed.{{cite news |url=http://www.irconnect.com/noc/press/pages/news_releases.html?d=39867 |title=Northrop Grumman Awarded NASA Contract for Next Generation Launch Technology |date=May 5, 2003 |accessdate=May 22, 2014 |publisher=Primezone}}

{{cite web |url=http://www.astronautix.com/engines/tr107.htm |title=TR-107 |publisher=Astronautix.com |accessdate=March 12, 2014 |url-status=dead |archiveurl=https://web.archive.org/web/20140805141204/http://astronautix.com/engines/tr107.htm |archivedate=August 5, 2014 }}

History

The TR-107 was developed by TRW following the successful conclusion of the development program for the TR-106 engine, a similar throttleable engine of about half the thrust burning LOX/LH2 instead of LOX / RP-1. Tom Mueller, then VP of Propulsion Development at Northrop, was project manager for both the TR-106 and TR-107 engines.

In 2002, Mueller co-founded SpaceX with Elon Musk and became the VP of propulsion{{cite web |url=http://www.spacex.com/about/leadership |title=Tom Mueller Bio |publisher=SpaceX |accessdate=May 21, 2014 |url-status=dead |archiveurl=https://web.archive.org/web/20140516101427/http://www.spacex.com/about/leadership |archivedate=May 16, 2014 }} after cancellation of the SLI program.{{cn|date=May 2014}}

Status

Northrop Grumman development of the TR-107 engine permitted consideration for potential use on next-generation launch and space transportation systems.

{{As of|2023}}, no flight models are known to exist.

See also

References

{{Reflist}}