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Environmental Impact Analysis Process

Environmental Impact Analysis Process
Author: United States. Department of the Air Force
Publisher:
Total Pages: 352
Release: 1979
Genre: Intercontinental ballistic missile bases
ISBN:

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MX: Milestone II. Final Environmental Impact Statement. Volume III. Missile Flight Testing

MX: Milestone II. Final Environmental Impact Statement. Volume III. Missile Flight Testing
Author: AIR FORCE SYSTEMS COMMAND WASHINGTON D C.
Publisher:
Total Pages: 456
Release: 1978
Genre:
ISBN:

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This volume describes the environmental consequences of system level Testing of the MX weapon system at Vandenberg Air Force Base, CA (VAFB) including ground tests and flight tests of the MX missile from an operational basing mode. Alternative missiles other than MX as described in Volume I are being considered for possible inclusion in the FSED and, therefore, flight testing at Vandenberg. The only significant variations in environmental impact to the Vandenberg area expected as a function of the alternative missiles being considered are related to the handling and launch safety considerations of a specific missile. The standard launch safety analysis and procedures currently in force for all missile assembly and launch tasks at Vandenberg will be adhered to for any missile selected for Full-Scale Engineering Development (FSED) and Flight Test at Vandenberg.


Ground-Based Midcourse Defense (GMD) Extended Test Range (ETR)

Ground-Based Midcourse Defense (GMD) Extended Test Range (ETR)
Author:
Publisher:
Total Pages: 850
Release: 2003
Genre: Ballistic missile defenses
ISBN:

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"The proposed action is to construct and operate additional launch and test facilities including the SBX in the Pacific Region, and to conduct more realistic interceptor flight tests in support of GMD development."--Page es-4


Environmental Impact Analysis Process Environmental Assessment PEGASUS Air Launched Space Booster

Environmental Impact Analysis Process Environmental Assessment PEGASUS Air Launched Space Booster
Author:
Publisher:
Total Pages: 106
Release: 1989
Genre:
ISBN:

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The Pegasus air-launched vehicle is part of the Advanced Space Technology Program of the Defense Advanced Research Projects Agency (DARPA). The program is designed to demonstrate high-payoff advanced technology to improve systems' operational support to military commanders. The government launch and demonstration of the privately developed Pegasus vehicle will be used to evaluate its launch flexibility and utility for support if military objectives as well as to place small experimental payloads into orbit. The Pegasus launch system is a three-stage solid-rocket-motor launch vehicle designed to be launched from a B-52B aircraft or similar large-lift aircraft, either government or private. It is being developed to provide a responsive, inexpensive, and highly mobile launch service to satisfy the launch needs of small mass 190km (425-lb) and volume 1.8 m 3 (65-fl 3) payloads for the U.S. Department of Defense and other users. The DARPA has contracted for Pegasus launch services for two captive flights and two launches into polar orbit with an option for four more flights. A B-52B carrying the Pegasus will take off from Edwards Air Force Base (AFB), north of Los Angeles, California, climbing toward the town of Paso Robles. The aircraft will turn northwest about 70 km (40 mi) east of San Luis Obispo, passing to within 7 km (4 mi) of Paso Robles. The B-52B makes another turn near the Farallon Islands to head south into the Western Test Range (WTR) about 160 km (100 mi) into the Pacific Ocean. Mission control for these operations will be at the NASA Ames Research Center/Dryden Flight Research Facility, Edwards AFB, California. This environmental assessment addresses the potential environmental impacts from he six potential DARPA/NASA launches and assumes that the configuration of the Pegasus and its use of the B-52B remain as described in this document.


MX: Milestone 2

MX: Milestone 2
Author:
Publisher:
Total Pages: 156
Release: 1978
Genre:
ISBN:

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