The Defense Advanced Research Projects Agency (DARPA) and the U.S. Air Force have selected teams for the first phase of the Force Application and Launch from the Continental U.S. (FALCON) program.
Nine contractors were selected for negotiations for Task 1 (Small Launch Vehicle) and three contractors were selected for negotiations for Task 2 (Hypersonic Weapon Systems).
Subject to successful negotiations, each contractor will conduct a six-month system definition study within its respective task. At the conclusion of Phase I, DARPA and the Air Force will decide whether to proceed with Phase II, which would be a 36-month design and development effort.
FALCON Phase I, Task 1 contractors will receive between $350,000 and $540,000 each for their Phase I effort. Task 1 contractors are listed below.
The fundamental underpinning of the technical approach to be taken in the FALCON program is the recognition that a common set of technologies can be matured in an evolutionary manner that will provide a near-term (circa 2010) operational capability for responsive, affordable smallsat spacelift and prompt global strike from the continental U.S. (or equivalent reach from alternative U.S. basing) while also enabling future development of a reusable Hypersonic Cruise Vehicle for the far-term (circa 2025).
In FALCON Phase I Task 1, contractors will develop conceptual designs, performance predictions, cost objectives, and development and demonstration plans for the Small Launch Vehicle (SLV). The SLV will provide a low-cost, responsive launch capability capable of placing a small satellite or other payload weighing approximately 1,000 pounds into a low Earth orbit at a total launch cost of less than $5,000,000 (excluding payload and payload integration costs).
In FALCON Phase I Task 2, contractors will develop conceptual designs, concepts of operations, and a demonstration plan and identify critical technologies for the Hypersonic Weapon Systems portion of the program, which includes the Common Aero Vehicle, the Enhanced Common Aero Vehicle, and the Hypersonic Cruise Vehicle.
The Common Aero Vehicle will be an unpowered, maneuverable, hypersonic glide vehicle capable of carrying approximately 1,000 pounds of munitions, with a range of approximately 3,000 nautical miles. The Enhanced Common Aero Vehicle would be a more advanced design that offered substantially greater range and improved maneuverability.
The reusable Hypersonic Cruise Vehicle will be an autonomous aircraft capable of taking off from a conventional military runway and striking targets 9,000 nautical miles distant in less than two hours.
DARPA is responsible for overall program management of the FALCON program. DARPA manages the program, with the Air Force Space Command Space and Missile Systems Center providing a deputy program manager. Representatives from Air Force Space Command Space and Missile Systems Center/Detachment 12, Air Force Space Command DR and the Air Force Research Laboratory provide technical assistance and support in conducting milestone reviews.
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Pad Abort Concept Demonstrates Stability in Wind Tunnel Testing
Denver - Nov 04, 2003
In wind tunnel tests during September and October, the Lockheed Martin-designed Pad Abort Demonstration (PAD) vehicle proved that it is stable under the maneuvering required to escape from a catastrophic launch vehicle event. The tests were conducted at Lockheed Martin's High Speed Wind Tunnel in Texas.
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