← Back to Patent Explorer
US3262655A Expired / Lapsed US ⏱️ 0.0 years remaining

Alleviation of divergence during rocket launch

Assignee: Individual
•
Filing: 1963-12-26
•
Granted: 1966-07-26
•
Expires: 1983-12-26
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

No abstract record available.

Inventors

  • 👤 Jr Warren Gillespie

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 08:41
CPC Classifications
F; F42; F42B; F42B10/00; F42B10/60; F42B10/62

Claims Analysis

Total Claims: 1
Claim 1
Independent Claim 67 words
A CONNECTION FOR A BOOSTER AND PAYLOAD OF A SPACE VEHICLE COMPRISED OF: LINK MEANS PIVOTALLY SECURED TO A PAYLOAD AND A BOOSTER, THE EXTENDED LONGITUDINAL CENTERLINES OF SAID LINKS CROSSING AT THE CENTER OF GRAVITY OF SAID PAYLOADS; AND STABILIZING MEANS ATTACHED TO SAID LINK MEANS AND TO SAID BOOSTER, WHEREBY THE MOMENT CAUSED BY TRANSVERSE AERODYNAMIC FORCES THAT IS APPLIED TO SAID BOOSTER IS REDUCED.

References Cited (Backward Citations)

US3126174A Cited
US2341726A Cited
US3195462A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1969-07-25 1970-01-24 1970-07-26 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1973-07-25 1974-01-24 1974-07-26 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1977-07-25 1978-01-24 1978-07-26 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag