NWC Advanced Common Intercept Missile (ACIMD)

[overscan (PaulMM)]

Often mentioned in relation to AAAM / AIM-152, this is actually the NWC (Naval Weapons Center) ACIMD, which was a prototype of a long range AAM concept.

 

[overscan (PaulMM)]

ADVANCED COMMON INTERCEPT MISSILE DEMONSTRATION PROGRAM (ACIMD)

The ACIMD program is a new start for FY-81. The general goals of this program are to design, build, and flight test a ramjet powered air-to-air missile. The principle objectives for the aerodynamics portion of the program are to: define the preliminary drag and lift based on prior Airbreathing Missile studies, use the propulsion system determined from the preliminary studies to determine an external configuration and aerodynamics of this configuration, and use wind-tunnel results and predictions to document the aerodynamics of the final configuration in preparation for a flight test program.

ANNUAL REPORT OF THE NAVY AEROBALLISTICS COMMITTEE TO THE NAVAL AIR SYSTEMS COMMAND AND THE NAVAL SEA SYSTEMS COMMAND FOR 1981

https://apps.dtic.mil/sti/tr/pdf/ADA112830.pdf

 

[overscan (PaulMM)]

See https://www.secretprojects.co.uk/threads/nwc-mcdonnell-douglas-aiaam-study.42821 and https://www.secretprojects.co.uk/threads/aim-152-aaam-phoenix-replacement-projects.2548 for related topics.

 

[NMaude]

Is there a link to any website and/or document(s) that go into detail on this study? I checked over at the wikipedia and while there's a mention in some articles there's no article on the study itself.

 

[overscan (PaulMM)]

NASA-TM-84557 Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations

Two tail configurations were investigated: a tri-tail and an X-tail. The tests included body-inlet, body-inlet-wing, body-inlet-tail, and body-inlet-wing-tail
configurations.

Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations - NASA Technical Reports Server (NTRS)

A series of air-breathing missile configurations was investigated to provide a data base for the design of such missiles. The model could be configured with either a single axisymmetric or a two dimensional inlet located at the bottom of the body. Two tail configurations were investigated: a...

ntrs.nasa.gov