Statement of Introduction Mr. Chairman and members of the Committee, it is an honor for me to appear before this Committee to address
the potential threat to our national security satellites posed by electromagnetic pulse (EMP). Before I address my
remarks to the topic of EMP, I would like to give you a brief background on the Deputy Under Secretary of
Defense (Space) (DUSD(Space)) and our responsibilities. This will assist in explaining the scope of our activities. DUSD(Space) is the Secretary's principal staff assistant for space matters. We are developing the plans and
architectures which will effectively lead us through the next decade. In this capacity we develop, coordinate and
oversee the implementation of DoD policies and guidance for military and intelligence space activities; oversee the
implementation of DoD space systems related strategy and plans; and, oversee DoD space mission and system
architectures, acquisition and technology programs. We are key in analyzing and implementing the National
Security Section of the National Space Policy and other Presidential space policies. We successfully lead the
Overarching Integrated Product Team (OIPT) for the Space-Based Infra-Red System keeping this major
acquisition program healthy and on track. We are currently leading OIPTs on the Evolved Expendable Launch
Vehicle (EELV) and the National Polar Orbiting Environmental Satellite System (NPOESS). In accomplishing these
tasks we coordinate and monitor the implementation of policies established by other DoD offices and agencies.
For example, electromagnetic pulse survivability policy and standards are established by the Office of the Assistant
to the Secretary of Defense (Nuclear, Chemical, Biological Defense Programs). These policies and standards are
included in space systems design and acquisition appropriate to the validated threat to the system. Hardening guidance is established by national and defense policy and the Joint Staff. Space systems are hardened
consistent with this guidance. We recognize the growth in the use of space systems as articulated in Joint Vision
2010. In light of this potential massive use of space capabilities, both national security and commercial systems will
require a review and study of critical infrastructure components. DUSD(Space) is heading this DoD-wide study. In the past, National Security Space Systems have been hardened to varying degrees. This variation continues
today. Hardening all systems to the maximum level incurs heavy cost penalties. We are studying a range of
protection measures which will enhance the entire satellite constellation. This review will look at these protection
measures with cost as an independent variable. The Joint Space Management Board (JSMB) received and
approved a comprehensive space protection study conducted by the DoD Space Architect and the National
Reconnaissance Office. Implementation of the recommendations contained in this study of current and projected
issues is being planned. Electromagnetic Pulse Effects on Space Systems As Dr. Ullrich of the Defense Special Weapons Agency has explained, the most common usage of the term
electromagnetic pulse (EMP) refers to the complex radio frequency waveform generated by a nuclear device being
detonated in the atmosphere (also known as High Altitude EMP, HEMP). This "transmission" can contain large
amounts of energy that can be "received" by a military or civilian system in unexpected ways that damage electrical
components. The process is somewhat similar to the static one picks up on an AM car radio during a thunderstorm
due to lightning. The amount of HEMP energy that "couples" to the system depends on many factors, specific
system design and distance from the source being among the most important. The car radio analogy is still
appropriate here with an FM radio being less disturbed and very distant lightning producing no static. Spacecraft
are far from a HEMP event and are not damaged. The effects of HEMP on satellite ground stations can be more
disruptive, and depend on a number of factors (e.g., altitude and distance of burst or design of ground station).
Military communications facilities such as the National Military Command Center have HEMP hardened facilities. Another "form" of electromagnetic pulse previously discussed is system generated EMP or SGEMP. This effect
happens only in a vacuum and when X-rays produced by a nuclear device strike a satellite and displace electrons
throughout the spacecraft. The movement of these electrons produces large currents in the satellite's structure and
electrical systems usually with detrimental effects. An analogy would be plugging a nine-volt transistor radio in a
household electrical socket. The amount of SGEMP generated in a spacecraft is dependent upon the nuclear
weapon's yield, X-ray spectrum, distance to the nuclear device and, most importantly, the design of the satellite.
The design and testing of military space systems for vulnerability to SGEMP effects is the responsibility of the
individual program offices. The adequacy of nuclear survivability features is an item that is considered by the
Defense Acquisition Board. As part of our ongoing space protection efforts, we will be looking explicitly at the
issue with cost as an independent variable. Radiation Hardened Microelectronics The "radiation effects," discussed by Dr. Ullrich, are the result of natural and man-made sources. Natural sources
are cosmic rays, charged particles trapped in the Van Allen belts and solar flares. Engineers design commercial and
civil satellite electronics to withstand this naturally occurring radiation. DoD satellite systems must be designed to
survive much more severe radiation environments induced either by hostile actions (JCS Level 1 hardening
requirements) or high ambient radiation orbits (Global Positioning System). The specially designed and
manufactured electronic components are termed to be "radiation hardened" or simply "Rad Hard." The availability
of Rad Hard electronic components is crucial to survivable DoD satellite systems and receives special attention
from DUSD(Space). In December 1996 an Integrated Product Team (IPT) chaired by the Assistant Deputy Under Secretary of Defense (Space Systems Acquisition) reported to the Under Secretary of Defense (Acquisition and Technology) on the industrial base that designs and manufactures Rad Hard components. The IPT found that:
The IPT's Rad Hard strategy was to generate economies of scale by providing the "seed money" for Rad Hard parts development and production thereby assisting the manufacturers to remain in the business while they develop a non-DoD market. The IPT specifically recommended:
In May 1997 the USD(A&T) approved the IPT's recommendations and directed a DoD wide initiative
implementing them. Detailed actions were assigned to DoD staff offices and to the Air Force. These tasks are
currently being accomplished with the establishment of the Radiation Hardened Electronics Oversight Council
being the highest priority. We will update the committee on the implementation of the DoD Rad Hard initiative and
the progress in creating an interagency coordination mechanism. These issues become more important as DoD transitions to dependence upon commercial satellite systems to provide cost effective ways of meeting mission requirements. We are studying this issue in conjunction with US Space Command and the NRO. The vulnerabilities of both National Security and commercial assets will have to be taken into account. To the extent we migrate critical space functions to commercial providers, we need to focus on protection and negotiate appropriate hardness levels. |
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