Patent US3083527A successfully refreshed from Google Patents.
US3083527A
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Hybrid rocket propulsion process
Assignee: Phillips Petroleum Co
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Filing: 1960-10-10
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Granted: 1963-04-02
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Expires: 1980-10-10
Abstract
No abstract record available.
Inventors
- 👤 Homer M Fox
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 11:04
CPC Classifications
F; F02; F02K; F02K9/00; F02K9/42; F02K9/60; F02K9/62; C; C06; C06B; C06B33/00; C06B33/02; C06B45/00; C06B45/04; C06B45/06; C06B45/10; C06B45/105; C06B47/00; C06B47/02; C06B47/08
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
46 words
THE METHOD OF INCREASING THE SPECIFIC IMPULSE DEVELOPED BY EJECTING FROM A ROCKET MOTOR THE GASEOUS PRODUCTS OF COMBUSTION OF A SOLID ROCKET PROPELLANT WHICH METHOD COMPRISES INCORPORATING A HIGH ENERGY FUEL COMPONENT SELECTED FROM THE GROUP CONSISTING OF ALUMINIUM, MAGNESIUM, SILICON, TITANIUM, BERYLLIUM, BORON, DECABO-
Claim 2
Independent Claim
46 words
THE METHOD OF INCREASING THE SPECIFIC IMPULSE DEVELOPED BY EJECTING FROM A ROCKET MOTOR THE GASEOUS PRODUCTS OF COMBUSTION OF A SOLID ROCKET PROPELLANT WHICH METHOD COMPRISES INCORPORATING A HIGH ENERGY FUEL COMPONENT SELECTED FROM THE GROUP CONSISTING OF ALUMINIUM, MAGNESIUM, SILICON, TITANIUM, BERYLLIUM, BORON, DECABO-
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1966-04-01 | 1966-10-01 | 1967-04-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1970-04-01 | 1970-10-01 | 1971-04-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1974-04-01 | 1974-10-01 | 1975-04-02 | $7700.00 | Window Closed / Lapsed |