Pulsed Integral Rocket.

Nagy,

Pulsed Integral Rocket.

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Abstract:

The prevention of over-acceleration of air-launched air-breathing missiles which are boosted by a solid fueled rocket is accomplished by replacing the solid refueled rocket with a two-section solid motor arrangement designed for a choice between simultaneous burning and sequential burning. When a host aircraft is flying are relatively low velocities, the two-section motors should be fired simultaneously to boost the ramjet of the air-breathing missile to operational velocities mach 3 to mach 5. When the host aircraft is flying at relatively high velocities, the two-section motors should be fired sequentially to aviod over-acceleration and extend the operational range of the missile. While the ramjet and the two-section rocket motor may all be housed in the same casing, they must be separated from each other by thermal insulation and must have their own igniter which is controlled separately.

Author(s):

Nagy,

Author Organization(s):

DEPARTMENT OF THE AIR FORCE WASHINGTON DC

Descriptive Note:

Patent Application,

Pagination:

0013

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release, Document Partially Illegible

Distribution Statement:

Availability: This Government-owned Invention Available For U.s. Licensing And, Possibly, For Foreign Licensing. Copy Of Application Available Ntis. Document Partially Illegible.

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

PAT-APPL-789 864

Subject Terms

Joint Capability Areas:

JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means

Modernization Areas:

Hypersonics

Communities of Interest:

Weapons Technologies

Descriptor(s):

*PATENT APPLICATIONS, *INTEGRAL ROCKET RAMJETS, *SOLID PROPELLANT ROCKET ENGINES, DUAL MODE, GUIDED MISSILES, AIR LAUNCHED, PULSES

Field(s)/Group(s):

Air- and Space-Launched Guided Missiles, Solid Propellant Rocket Engines

Keyword(s):

*Pulsed integral rocket motors

Report Date:

1985 Oct 21