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US3462952A Expired / Lapsed US ⏱️ 0.0 years remaining

Rocket propulsion process using irradiated solid polymeric propellant

Assignee: Dal Mon Research Co
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Filing: 1958-12-05
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Granted: 1969-08-26
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Expires: 1978-12-05
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Abstract

No abstract record available.

Inventors

  • 👤 Gaetano F D Alelio

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-09 03:09
CPC Classifications
C; C08; C08F; C08F291/00; C08F291/18; C10; C10L; C10L5/00

Claims Analysis

Total Claims: 1
Claim 1
Independent Claim 59 words
A PROCESS FOR PROPELLING A ROCKET COMPRISING THE STEP OF COMBUSTING AN IRRADIATED, METAL-CONTAINING COMPOSITION CONSISTING ESSENTIALLY OF AT LEAST ONE HIGH MELECULAR WEIGHT HYDROCARBON MATERIAL HAVING A MOLECULAR WEIGHT OF AT LEAST 300, CONTAINING AT LEAST 15 PERCENT ALIPHATIC PORTION THEREIN, AND HAVING A PLURALITY OF REPEATING UNITS THEREIN HAVING A FORMULA SELECTED FROM THE CLASS CONSISTING OF

References Cited (Backward Citations)

GB665262A Cited
US2796411A Cited
US2796529A Cited
US2942116A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1972-08-25 1973-02-24 1973-08-26 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1976-08-25 1977-02-24 1977-08-26 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1980-08-25 1981-02-24 1981-08-26 $7700.00 Window Closed / Lapsed

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