Madam Speaker, pursuant to the Republican Leadership standards on earmarks, I am submitting the folio information regarding earmarks I received as part of H.R. 2638, the Consolidated Security, Disaster Assistance, and Continuing…
Madam Speaker, pursuant to the Republican Leadership standards on earmarks, I am submitting the folio information regarding earmarks I received as part of H.R. 2638, the Consolidated Security, Disaster Assistance, and Continuing Appropriations Act, 2009, Section 2, Division C:
Project Name: Transportable Cryofracture/Plasma Arc.
Account: RDT&E, A.
Amount: $1,600,000.
Requesting Entity: General Atomics, 3550 General Atomics Ct., San Diego, CA 92816.
Description: The Transportable Cryofracture/Plasma Arc project is developing a system for the demilitarization of obsolete conventional munitions that combines two existing fixed-site technologies, cryofracture and plasma arc, into a tractor trailer mounted system that meets all National Highway Transportation and Safety Administration, NHTSA, and Federal Highway Administration, FHA, guidelines for size, weight, and safety. Using this technology to demilitarize munitions at their storage areas will be safer, more secure, much cheaper, and meet environmental emission standards.
Spending Plan: Of the $1,600,000 appropriated, $1,500,000 will be spent in the second quarter of Fiscal Year, FY09, 2009 to complete procurement of the demonstration system, $1,000,000 for materials and $500,000 for labor. $100,000 will be spent in the third quarter of FY09 for the same purpose, labor.
Project Name: Hydrocarbon Boost Technology Demonstrator.
Account: RDT&E, AF.
Amount: $1,400,000.
Requesting Entity: Aerojet-General Corporation, P.O. Box 13222, Sacramento, CA 95813.
Description: This program was initiated by the United States Air Force to meet its projected launch needs for the future. Upon completion, the demonstrator will provide technologies that will lead to a liquid engine that is inherently higher performing, more operable, and more affordable that any other U.S. engine. The use of lower-toxic hydrocarbon fuel also promises long-term savings for the Air Force in operation and maintenance costs. Since the Federal Government is the primary end-user, it is logical that Federal funding support the initiative.
Spending Plan: The FY09 $1,400,000 increase is to return the FY09 funding closer to the planned level at contract initiation. The total project is a $109 million/9 year program, and the 2009 funds are intended for Ox rich preburner and turbopump concept designs.
Project Name: Strike Weapon Propulsion (SWEAP).
Account: RDT&E, N.
Amount: $2,400,000.
Requesting Entity: Aerojet-General Corporation, P.O. Box 13222, Sacramento, CA 95813.
Description: The Nation is investing in the development of high-speed weapons that can engage time critical targets at ranges up to 600 nautical miles within 5 to 10 minutes. The required propulsion system operates at temperatures typically exceeding 3,000 to 4,000 degrees Fahrenheit, hotter than conventional rockets and ramjets, requiring advancement in the development of ceramic composite materials. Solutions to this challenge have been demonstrated; however, affordability is the remaining issue. The Strike Weapon Propulsion program's objective is to lower the cost of producing the structure for a High-Speed Strike Weapon Propulsion system by 80 percent. If the effort is not funded, the high speed strike capability will not be of benefit to the future war fighter because it will not be affordable. Other, less effective systems would then prevail based on their lower unit costs.
Spending Plan: The total project will be financed as follows: $1.7 million for the design of ceramic matrix engine structures; $1.8 million for subscale hardware fabrication; $0.5 million for subscale hardware testing; $2.2 million for full-scale combustor fabrication; and $0.8 million for combustor assembly and testing.
Project Name: Validation of Lift Fan Engine Systems.
Account: RDT&E, N.
Amount: $2,000,000.
Requesting Entity: Rotordynamics-Seal Research, 3302 Swetzer Rd., Loomis, CA 95650.
Description: This technology demonstration program will provide benefits to all citizens of the U.S. through the reduction in tax revenues necessary to maintain the fleet of engines for the Joint Strike Fighter aircraft. In addition, a new virtual testing capability will be created that has applicability to a wide range of commercial and aerospace systems leading to significant development cost reductions. The near-term specific task to be executed under this effort is development and experimental validation of Rotordynamics-Seal Research's RAPPIDTM virtual testing modeling and simulation software for analysis of lift fan engines with clutches, gears, and splines. RAPPIDTM is a flexible software package for the simulation of propulsion, power, and vehicle systems that enables faster and more accurate evaluation of new systems. For large projects, RAPPIDTM helps program managers plan their resources more wisely and efficiently to enable more cost certainty. The focus of the task is to complete development of software modules necessary for full lift fan engine simulations, to generate test data testing critical components that affect engine vibration characteristics, clutches, gears, and splines, and to use the generated data to validate the resulting software. This is proposed as a 2 year effort. The first year, needed software modules will be developed and validated against existing data and required design modifications will be completed to an existing test facility. In the second year, new validation data will be obtained for the dynamic characteristics of critical components and the validation of the software will be completed. Advanced modeling and simulation software has been developed for determining the remaining life of critical Joint Strike Fighter lift fan engine clutch, gear, and drive train components. This program will extensively validate the key models used in the software through experimentation. The existing test facility developed for this purpose has ``best in the world'' capabilities for measurement of difficult to obtain data sets. This validation will enable engine life assessment modeling tools to be verified for release for fleet management purposes.
Spending Plan: The total project cost is $5 million, of which $4.5 million will be used for
labor, six Ph.D. engineers, four M.S. engineers and four B.S. engineers, and $500,000 will be used for test hardware.