Abstract Disclosed is a flight simulator for missiles. The system comprises means for directing heat toward the nose cone of a missile while simultaneously imparting axial rotation to the missile. Both the heat and the axial rotation are programmed to conform to actual inflight heat and spin conditions and the cycle of simultaneous heat and rotation is programmed to conform to such inflight conditions. Means are also provided for monitoring the proper fuse function at any given time during the simulated flight and for recording the entire cycle of simulated flight. The programmer can be programmed for the full real flight time of a missile such that the time-speed relationship can be matched to that of any real or proposed flight.
Inventors
👤 Charles W. H. Barnett
👤 George K. Lucey, Jr.
👤 Douglas R. Augustine
Bibliographic Details
Application Number—
JurisdictionUS
Data Sourcegoogle_patents
Last Synchronized2026-10-25 08:20
CPC Classifications
F; F42; F42C; F42C21/00; G; G01; G01N; G01N17/00
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
120 words
A flight simulator for missiles having a nose cone and a fuse body comprising: means for directing heat towards the nose cone of said missile; means for monitoring the temperature of said nose cone and providing a feedback signal to adjust the application of said heat to the desired level; means for imparting axial rotation to said missile simultaneously with the application of said heat; means for monitoring the spin rate of said fuse and providing a feedback signal to adjust the application of said rotation to the desired level; means for programming the cycle of simultaneous heat and rotation to conform to in-flight conditions; and means for monitoring the fuse function at any given time during the simulated flight.
Claim 2
Dependent Claim
120 words
A flight simulator for missiles having a nose cone and a fuse body comprising: means for directing heat towards the nose cone of said missile; means for monitoring the temperature of said nose cone and providing a feedback signal to adjust the application of said heat to the desired level; means for imparting axial rotation to said missile simultaneously with the application of said heat; means for monitoring the spin rate of said fuse and providing a feedback signal to adjust the application of said rotation to the desired level; means for programming the cycle of simultaneous heat and rotation to conform to in-flight conditions; and means for monitoring the fuse function at any given time during the simulated flight.
Claim 3
Dependent Claim
21 words
The invention defined in claim 1 further comprising means for recording the cycle of heat and rotation during the simulated flight.
Claim 4
Dependent Claim
27 words
The invention defined in claim 1 further comprising means for exhausting heated air in the vicinity of the nose cone to facilitate rapid changes of heat conditions.