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US3302890A Expired / Lapsed US ⏱️ 0.0 years remaining

Rocket nozzle

Assignee: Atlantic Research Corp
•
Filing: 1964-07-10
•
Granted: 1967-02-07
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Expires: 1984-07-10
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Abstract

No abstract record available.

Inventors

  • 👤 Silver Bernard

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 08:10
CPC Classifications
F; F02; F02K; F02K9/00; F02K9/80

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 164 words
IN COMBINATION, A ROCKET MOTOR AND AN AXIAL-THRUST MODULATING ROCKET EXHAUST NOZZLE COMPRISING: (A) A HOUSING INCLUDING A PAIR OF END WALLS, A FIRST AND A SECOND CHAMBER WITHIN SAID HOUSING, SAID FIRST AND SECOND CHAMBERS BEING SEPARATED BY A PARTITION HAVING AN OPENING THERETHROUGH, ONE OF SAID END WALLS HAVING A REARWARDLY DIRECTED PRIMARY EXHAUST PORT THERETHROUGH COMMUNICATING WITH SAID FIRST CHAMBER, SAID HOUSING HAVING A LATERALLY DIRECTED SECONDARY EXHAUST PORT THERETHROUGH COMMUNICATING WITH SAID SECOND CHAMBER, (B) FIRST MEANS MOUNTED WITHIN SAID HOUSING FOR VARYING THE EFFECTIVE EXHAUST AREA OF SAID PRIMARY EXHAUST PORT, AND (C) SECOND MEANS MOUNTED WITHIN SAID HOUSING FOR VARYING THE EFFECTIVE EXHAUST AREA OF SAID OPENING IN INVERSE PROPORTION TO THE VARIATION OF SAID PRIMARY EXHAUST PORT AREA, THE GEOMETRICAL CONFIGURATION OF SAID PRIMARY EXHAUST PORT, SAID FIRST MEANS, SAID OPENING, AND SAID SECOND MEANS PROVIDING A CONSTANT SUM TOTAL EFFECTIVE EXHAUST AREA TO EFFECT VARIOUS AXIAL THRUST LEVELS WITHOUT AFFECTING THE ROCKET MOTOR COMBUSTION CHAMBER PRESSURE.
Claim 2
Dependent Claim 164 words
IN COMBINATION, A ROCKET MOTOR AND AN AXIAL-THRUST MODULATING ROCKET EXHAUST NOZZLE COMPRISING: (A) A HOUSING INCLUDING A PAIR OF END WALLS, A FIRST AND A SECOND CHAMBER WITHIN SAID HOUSING, SAID FIRST AND SECOND CHAMBERS BEING SEPARATED BY A PARTITION HAVING AN OPENING THERETHROUGH, ONE OF SAID END WALLS HAVING A REARWARDLY DIRECTED PRIMARY EXHAUST PORT THERETHROUGH COMMUNICATING WITH SAID FIRST CHAMBER, SAID HOUSING HAVING A LATERALLY DIRECTED SECONDARY EXHAUST PORT THERETHROUGH COMMUNICATING WITH SAID SECOND CHAMBER, (B) FIRST MEANS MOUNTED WITHIN SAID HOUSING FOR VARYING THE EFFECTIVE EXHAUST AREA OF SAID PRIMARY EXHAUST PORT, AND (C) SECOND MEANS MOUNTED WITHIN SAID HOUSING FOR VARYING THE EFFECTIVE EXHAUST AREA OF SAID OPENING IN INVERSE PROPORTION TO THE VARIATION OF SAID PRIMARY EXHAUST PORT AREA, THE GEOMETRICAL CONFIGURATION OF SAID PRIMARY EXHAUST PORT, SAID FIRST MEANS, SAID OPENING, AND SAID SECOND MEANS PROVIDING A CONSTANT SUM TOTAL EFFECTIVE EXHAUST AREA TO EFFECT VARIOUS AXIAL THRUST LEVELS WITHOUT AFFECTING THE ROCKET MOTOR COMBUSTION CHAMBER PRESSURE.

References Cited (Backward Citations)

DE860754C Cited
US2509238A Cited
GB723160A Cited
US2933889A Cited
US3177655A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1970-02-06 1970-08-08 1971-02-07 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1974-02-06 1974-08-08 1975-02-07 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1978-02-06 1978-08-08 1979-02-07 $7700.00 Window Closed / Lapsed

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