Missile test method for testing the operability of a missile from a launch site

• US 5,721,680 A
• Filed: 06/07/1995
• Issued: 02/24/1998
• Est. Priority Date: 06/07/1995
• Status: Expired due to Term

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Hughes Missile Systems Company
• Inventors: Monk, R. Winston, Van Cleve, David P.
• Primary Examiner(s): LOUIS JACQUES, JACQUES H
• Application Number:
  US08/478,148
• Time in Patent Office: 993 Days
• Field of Search: 364/424.03, 364/423, 364/578, 364/550, 364/55.01, 324/73.1, 244/3.24, 244/3.21, 244/3.1, 244/3.15, 244/3.16, 244/3.11, 244/3.12, 244/3.13, 244/3.14, 244/3.19, 244/3.2, 244/3.22, 89/1.14, 89/1.11, 89/1.814, 89/1.819, 89/1.8, 89/1.81, 102/378, 102/498, 102/293, 102/388, 102/215-218, 434/21, 434/12, 434/22, 434/11, 434/14, 73/167, 73/865.6
• US Class Current: 701/3
• CPC Class Codes: F41G 7/001 Devices or systems for testing or checking

Abstract

A missile is tested by first stimulating the performance of missile built-in tests that are stimulated in service by signals from the launch site, and which tests do not require internal access to the missile. If performance is satisfactory, no further testing is required. If a condition of unsatisfactory missile performance is detected, an access cover is removed, connections are made to internal sources of data, and the built-in tests are repeated in order to determine which internal components caused the unsatisfactory missile performance. The component is repaired. The testing with the access cover removed is repeated, and, if the performance is satisfactory, the access cover is replaced and the testing with the access cover present is repeated.

Claims

1. A method for testing the operability of a missile during service operation, comprising the steps of:

providing said missile that, during service operation, is to be launched from a launch site, the missile having

at least two internal component sections and a wiring harness communicating therebetween, there being at least two cover-off missile connectors, one for each of said at least two internal component sections being accessible only when a missile access cover is removed,

an external missile umbilical connector that, during service operation, communicates with the launch site prior to launching of said missile, and

a missile data-link receiver that, during service operation, communicates with the launching of said missile site after launch;

providing an external test apparatus comprising

a test controller,

at least two test cover-off component-level test lines, one for each of the at least two cover-off missile connectors, each of said at least two cover-off component-level test lines having a first end m communication with the test controller and a second end having a cover-off component-level test line connector to mate with a respective one of the at least two cover-off missile connectors,

an umbilical line having a first end in communication with the test controller and a second end having a test apparatus umbilical connector to mate with the external missile umbilical connector,

a test apparatus data-link transmitter in communication with the test controller,

a power supply that provides to the test controller power levels available to the missile from the launch site during service operation, and

a pneumatics supply controlled by the test controller, the pneumatics supply being operated to pneumatically unlock and to allow operation of electromechanical components of the missile;

performing a cover-on test sequence by

an operator connecting the test apparatus umbilical connector to the external missile umbilical connector,

the operator positioning the test apparatus data-link transmitter in a position to communicate with the missile data link receiver,

the test controller stimulating performance of missile built-in tests through the umbilical line and the missile data-link receiver, and

the test controller evaluating the results of the missile built-in tests to determine the presence of an unsatisfactory missile test performance; and

, in the event of the detection of an unsatisfactory missile performance; and

performing a cover-off test sequence by

the operator removing the missile access cover,

the operator connecting each cover-off component-level test line connector to the respective cover-off missile connector, and

the test controller stimulating performance of missile built-in tests through the umbilical line and the missile data-link receiver and gathering data through the test apparatus cover-off component-level test lines, and

the test controller evaluating the results of the missile built-in tests to isolate the cause of an unsatisfactory missile performance at a component level.

2. The method of claim 1, including an additional step, after the step of performing the cover-off test sequence, of

the operator repairing at least one component of the missile.

3. The method of claim 2, including the additional steps, after the step of the operator repairing, of

performing a second cover-off test sequence by

the test controller stimulating performance of missile built-in tests through the umbilical line and the missile data-link receiver and gathering data through the test apparatus cover-off component-level test lines, and

the test controller evaluating the results of the missile built-in tests to determine if the cause of the unsatisfactory missile performance at the component level has been corrected, and, if the cause of the unsatisfactory missile performance at the component level has been remedied,

the operator disconnecting each cover-off component-level test line connector from the respective cover-off missile connector, and

the operator replacing the missile access cover.

4. The method of claim 3, including the additional steps, after the step of performing a cover-off test sequence, of

performing a second cover-on test sequence by

the test controller stimulating performance of missile built-in tests through the umbilical line and the missile data-link receiver,

the test controller evaluating the results of the missile built-in tests to determine whether the cause of the unsatisfactory missile test performance has been corrected, and, in the event that the cause of the unsatisfactory missile test performance has been corrected;

an operator disconnecting the test apparatus umbilical connector from the external missile umbilical connector; and

the operator removing the test apparatus data-link transmitter from a position to communicate with the missile data link receiver.

5. The method of claim 1, wherein in the step of providing said missile

said missile includes a guidance section, a control section, and the wiring harness extending therebetween.

6. The method of claim 5, wherein the step of performing a cover-off test sequence includes the step of

monitoring a telemetry built-in test data stream from the guidance section.

7. The method of claim 5, wherein the step of performing a cover-off test sequence includes the step of

simulating a launch cycle.

8. The method of claim 5, wherein the step of performing a cover-off test sequence includes the steps of

utilizing the pneumatic source to unlock a control surface of the control section, and

the test controller for monitoring the movement of the control surface.

9. The method of claim 5, wherein the step of performing a cover-off test sequence includes the steps of

performing a continuity check of the wiring harness.

10. The method of claim 1, wherein in the step of providing said missile

said missile, during service operation, is launched from an aircraft.