Separation Characteristics of the MK-20 (Rockeye) Laser-Guided Dispenser Munition from the F-4C Aircraft at Mach Numbers from 0.66 to 0.90
Abstract
Wind-tunnel tests were conducted using 0.05-scale models to investigate the separation characteristics of the MK-20 Laser-Guided Rockeye Munition (GRM) from the F-4C aircraft. The separation trajectories were initiated from the right-wing inboard pylon utilizing the Triple Ejection Rack and from single carriage positions on the right-wing inboard and outboard pylons. Captive-trajectory store separation data were obtained at Mach numbers from 0.66 to 0.90 for parent-aircraft level flight and 45-deg dive angle at a simulated altitude of 5000 ft. Freestream force and moment data were also obtained for the GRM with fins folded and deployed at Mach numbers from 0.66 to 0.90 at store angles of attack from -6 to 24 deg. For the time period of the trajectories obtained, the store separated from the parent aircraft without store-to-parent contact. Trajectory termination was usually a result of limitations imposed by the travel limits of the store support system or a balance load limit.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1971
- Accession Number
- AD0886753
Entities
People
- J. R. Myers
Organizations
- Arnold Engineering Development Complex