See details. Buy It Now. Add to cart. Be the first to write a review. About this product Product Information Develops a new metric for measuring the effect of operations tempo on the readiness of the mobility air forces The authors provide a new metric--the mission-day--to assess the ability of the mobility air forces MAF to conduct missions, train its forces, and maintain readiness.
The mission-day metric measures the availability of crewmem bers to fly missions while continuing training and other activities. It can detect problems arising from the operations tempo of MAF personnel as they take part in major theater operations and support U.
Additional Product Features Author s. Show more Show less. No ratings or reviews yet. Best-selling in Non-Fiction Books See all. Graphics must be distinguishable in black and white. Please virus-check your submissions. In the Air Force program, the outside investment funding must be from a government source, usually the Air Force or other military service. Should the requirements change, all Phase I awardees that are invited to submit Phase II proposals will be notified.austinyoganews.com/1819-the-best-smartphone.php
Measuring the Tempo of the Mobility Air Forces: TRAF | Angus & Robertson
The primary focus of the Phase I effort is to demonstrate the feasibility of developing, integrating and transitioning innovative process technologies in a manufacturing environment to support the production of inline materials for advanced weapon system s. For this effort, Phase I objectives are to define the requirements to establish an initial measurement capability to nondestructively measure and characterize inline thin film mat material in a production environment to ensure specification compliant materials are being produced.
In addition to demonstrating the proposed technology solution, successful offerors should also consider the technical, business and transition activities necessary to lower the risk of technology insertion into the integration processes of a joint service weapon system. The Phase I effort will identify and provide a proof of feasibility concept and a plan for the overall system concept and architecture. Phase I results must demonstrate a technical solution meet ing all program end requirements.
Submission of a Phase II proposal will be by invitation only.
At that time, special instructions will be provided for proposal preparation. For this effort, Phase I objectives are to define the requirements to establish an initial measurement capability to accurately and rapidly identify, characterize and register the defects to the aircraft coordinates.
Phase I contract s will be executed at an accelerated pace, a seven- month effort, including four months for technical effort and an additional three months for reporting. Also, the Phase II proposal must include both business and transition plan s. Air Force Program Manager Listing. Topic Number. Program Manager. AF thru AF Air Vehicles Directorate. Larry Byram. Directed Energy Directorate. Danielle Lythgoe. Human Performance Wing. Sabrina Davis. Information Directorate.
Rome NY Janis Norelli. Space Vehicles Directorate. Munitions Directorate. Suite Shirley Schmieder. Debbie Shaw. Sensors Directorate. Claudia Duncan. Julie Harris.
Propulsion Directorate. Mary Kruskamp. Barb Scenters. Propulsion Directorate West. Angela Harris. AF thruAF Ramsey Sallman. Arnold Engineering Development Center. Dhruti Upender. Air Force Flight Test Center. Bldg 1, Rm A. Abe Attachbarian. Oklahoma City Air Logistics Center. Becky Medina. Ogden Air Logistics Center. John Jusko. Warner Robins Air Logistics Center. Frank Zahiri. JSF Aircraft and Simulation. Review Suite for Cyber Warfare Training. Deployable Antennas. Materials Systems. Support Radar and Software Analysis. Handheld Devices. Array Antennas. Systems in Harsh Environments.
Fatigue LCF Life. Characteristics, Cost, and Throughput. Presence of Chelating Substances.
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Electronic Warfare EW systems. As such, export-controlled data restrictions apply. In addition, this acquisition involves technology with military or space application. Therefore, only U. The Air Force Research Laboratory, through its Pathfinder program, is leveraging these emerging concepts to demonstrate enabling technologies for a next generation Reusable Boost System RBS , including hypersonic flight with vehicle dry weights of only a few thousand pounds.
The goal of this SBIR project is to leverage these investments and techniques to design small, high performance experimental airbreathing vehicles that can be affordably fabricated and tested. There is a desire to drive the trend downward in both size and cost where practical.
Measuring the Tempo of the Mobility Air Forces: TR-150-AF
Other changes that delivered savings include opting to use weapons ranges such as Woomera in Australia and PMRF in Hawaii for launches as opposed to man-rated launch ranges such as Cape Canaveral in Florida. Additionally, the use of sounding rockets to boost the flight research vehicles FLiRVs , instead of ICBM class rockets, is contributing to cost savings. The development time needed to get to the first launch is also trending downward. As the overall scale of the effort comes down from the demonstration level X to the flight experiment level HIFiRE , the time to get to the first launch has been reduced from years to years.
Approaches to flight testing the vehicle s developed in the present effort shall address the viability of technology transition. Air-launched or ground-launched approaches must include realistic estimates for costs, including range costs, costs of flight-readiness and safety reviews, and costs associated with hardware modifications to ensure a successful flight testing program after Phase II.
It is the responsibility of the offeror to build a strong case for follow-on flight testing. It is not required for the flowpaths to be shared between the two propulsion systems, although it may be beneficial. Similarly, a clear understanding of the technology is essential. Demonstrating these technologies at small scale is very challenging and in some cases not practical.
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Offerors may seek to design and fabricate an entire stage or only critical components. Identify system level and technology applications of the proposed innovation. As a threshold, the vehicle can include multiple stages, but the goal is to have the entire propulsion cycle and flight vehicle in single stage. Demonstrate the experimental hardware or component prototypes developed in Phase I.