By Sir James Moncrieff Grierson
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V&V are interrelated and are accomplished throughout the systems engineering process and include lifecycle support and sustainment. Together, V&V demonstrate that the AMD system meets the mission need, design goals, and stakeholder expectations. This is referred to as the mission objectives. 1 Verification The SEMP should describe how verification is used to ensure that the AMD design satisfies the mission objectives. It is a continuing process that encompasses the verification of CONOPS, the architectural design, and the requirements.
Surface shaping causes the energy in the transmitted radar pulse to be reflected in other directions and not directly back to the radar, causing the energy in the radar return to be reduced. The offensive missile can also use composite materials that absorb radar energy to reduce their radar cross section. Other techniques related to the offensive missile seeker involve tilting the seeker when it is not active and the use of a seeker radome constructed of a frequency selective surface (FSS). Tilting the seeker will reduce the in-band forward aspect radar cross section.
This scenario is judged Missile Defense Problem 27 to be a worst-case scenario from an engagement timeline perspective. Most defensive systems do not have the ability to engage multiple offensive missiles in azimuth simultaneously. This is due to several reasons. All offensive missiles in the raid will not be detected simultaneously due to radar search patterns and the stochastic nature of the detection process. Usually, weapons can only be launched one at a time at an interval determined by the missile launcher salvo time.
