F41A 1/02

Hypervelocity missile propulsion using successive means for increasing the propulsive force

Official title: Hypervelocity missile propulsion using successive means for increasing the propulsive force, e.g. using successively initiated propellant charges arranged along the barrel length; Multistage missile propulsion

F41A1/02 (Hypervelocity missile propulsion using successive means for increasing the propulsive force) appears on 52 US grants and 35 published applications in this corpus.

Search patents in F41A
Granted patents
52
Published applications
35
Assignees
22
Inventors
57
Latest grant
18 Aug 2026

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F41A 1/02: granted patents and published applications per publication year
YearGranted patentsPublished applications
197710
197800
197900
198000
198100
198200
198300
198400
198500
198610
198700
198800
198900
199010
199130
199230
199310
199410
199500
199600
199700
199810
199900
200010
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200401
200500
200611
200700
200820
200902
201031
201110
201202
201311
201422
201513
201645
201753
201821
201924
202051
202101
202210
202333
202411
202533
202620

By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.