Space X stopped by infringement of Rocketdyne RL10 Engine

All know lunches in pass and future commonly called Space X is stopped from Antitrust over Rocketdyne RL10 Engine by "The Pentagon" such Military to issue of Domestic Profit is beyond the use of Space Travel example in theft of Rocketdyne engine RL10 Engine founded when both The Pentagon and NASA (A Legislation Administration of International use of Space in 1959 as of yet no construction byby NASA has ever token place) refuse to allow patent of Rocketdyne engine RL10 Engine toto go foreward but Space X took and redesign with out rights of Rocketdyne is simple theft the arguments counter in Congress with disrespect of the Patent Rights Reserve to Rocketdyne then use of Today as like Landing didn't happen the RL10 Engine is the foundation of the Saturn Lunch to the Moon and many after such review a Criminal approach argument to steal such Authority of Rocketdyne and in Closing is Rocketdyne Rights of Space Travel Today that story is very different. There are avionic
systems, hardware systems, manufacturing tools and techniques
readily available for use in low-Earth orbit. The ISS has
developed the techniques needed for sustained human presence
with reasonable risk in low-Earth orbit. However, the highly
reliable and maintainable systems necessary for beyond low-
Earth orbit do not yet exist, and NASA is focused on developing
these systems. The ISS is being used to test and refine many of
these systems needed for beyond low-Earth orbit. The new
challenge for NASA is to develop these new techniques and
systems for beyond low-Earth orbit.
NASA must also use the ISS national laboratory
activity to expose commercial industry to the advantages of
space-based research for terrestrial applications.
United Launch Alliance (ULA);
The anomaly caused delays to forthcoming Atlas V and Delta IV launches, due to the common RL-10 upper stage engines. The fault was traced to a new type of valve being used in place of an older component which had gone out of production. To resolve the problem, the older design was put back into production, and in the meantime, surplus valves from the original production run were used.
RL-10 upper stage engines
RL10 Engine
The remarkable RL10 has accumulated one of the most impressive lists of accomplishments in the history of space propulsion. Created in 1959, after our engineers harnessed high-energy liquid hydrogen as fuel for aerospace propulsion, the RL10 has helped place numerous military, government and commercial satellites into orbit, and powered space-probe missions to nearly every planet in our solar system. Some of its notable interplanetary missions include the Surveyor Lunar Lander, Viking Mars Lander and the Voyager Outer Planets Fly-By, while its heritage includes supporting MILSTAR, EUTELSAT, TDRS ECHOSTAR, INTELSAT, GALAXY, DSCSIII, and JCSAT satellites.

Today, the RL10 continues its legacy as the industry workhorse, with two separate models supporting the latest versions of United Launch Alliance's (ULA) launch vehicles. The RL10A-4-2 powers the upper stage of the Atlas V, and the RL10B-2 powers the upper stage of the Delta IV.

The RL10B-2 also features the world's largest carbon-carbon extendible nozzle. This high-expansion ratio nozzle enables the RL10B-2 to achieve 465.5 seconds of specific impulse and lift payloads of up to 30,000 lbs.

Program Milestones

Global Positioning System (GPS) Block IIF navigation satellite for the U.S. military
Third-generation Tracking and Data Relay Satellite (TDRS-L) for NASA
The Mobile User Object System (MUOS-2) satellite for the U.S. Navy
Specifications

RL10A-4-2 Engine

Propellants: Fuel= Hydrogen; Oxidizer= Liquid Oxygen
Provides 16,500–22,300 pounds of thrust
Specific impulse in vacuum 444.4–451.0 sec; mixture ratio: 5.1–5.5:1
Weight: 310–370 lb
RL10B-2 Engine

Propellants: Fuel= Liquid Hydrogen; Oxidizer= Liquid Oxygen
Provides 24,750 pounds of thrust
Specific impulse in vacuum 465.5 sec; mixture ratio: 5.88:1
Weight: 664 pounds
RL10 Engine by Rocketdyne

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