Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy
First Claim
1. A system for reducing plasma induced communication blackout during reentry, comprising:
- a reentry vehicle having a biconic nose, a base opposite the biconic nose, a communication antenna on the base, and a plurality of flaps configured to provide 3-axis steering capability;
an electrophilic gas injectant; and
an electrophilic gas injection system having at least one exit port in the base for injecting the electrophilic gas injectant into plasma near the communication antenna to reduce free electrons in the plasma.
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Accused Products
Abstract
A system for reducing plasma induced communication disruption is disclosed. The system utilizes an electrophilic gas injectant, bent reentry vehicle nose shaping and a number of flaps configured to provide 3-axis steering capability. Injecting electrophilic gas injectant into plasma accomplishes reduction of plasma induced communication disruption by removing free electrons in the plasma which causes the communication disruption. For reentry vehicles, a bent biconic nose also reduces plasma effect during reentry. By combining electrophilic gas injection and bent nose shaping, the system reduces and/or eliminates plasma induced communication disruption, such as, GPS communication blackout, for a reentry vehicle during reentry. Furthermore, the 3-axis steering capability renders the reentry vehicle more maneuverable. Performance of the reentry vehicle during reentry, such as, target accuracy, is thus improved.
44 Citations
5 Claims
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1. A system for reducing plasma induced communication blackout during reentry, comprising:
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a reentry vehicle having a biconic nose, a base opposite the biconic nose, a communication antenna on the base, and a plurality of flaps configured to provide 3-axis steering capability; an electrophilic gas injectant; and an electrophilic gas injection system having at least one exit port in the base for injecting the electrophilic gas injectant into plasma near the communication antenna to reduce free electrons in the plasma. - View Dependent Claims (2, 3, 4, 5)
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Specification
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- Resources
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Current AssigneeLockheed Martin Corporation (Martin Marietta Corporation)
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Original AssigneeLockheed Martin Corporation (Martin Marietta Corporation)
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InventorsMeyer, J. William, Teter, Roger D., Dunn, Steven A.
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Primary Examiner(s)Holzen; Stephen A.
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Application NumberUS10/990,393Time in Patent Office1,027 DaysField of Search244/158.9, 244/159.1, 244/171.7, 244/171.8, 244/158.1US Class Current244/159.1CPC Class CodesB64G 1/62 Systems for re-entry into t...
