Solid body equations to calculate the trajectory of ramjet
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Authors
Imai, Kenji
Advisors
Second Readers
Subjects
Six-degree-of-freedom trajectory
ramjet projectile
exterior ballistics
gun launched
ramjets
ramjet projectile
exterior ballistics
gun launched
ramjets
Date of Issue
1982-04
Date
1982-04
Publisher
Monterey, California. Naval Postgraduate School
Language
Abstract
Six-degree-of-freedom trajectory equations for a ranrjet propelled,
gun launched projectile are formulated. An outline for FORTRAN computer
program flow charts also appear in the report. Special emphasis is given
to the effect of wind on trajectory errors.
Type
Technical Report
Description
Series/Report No
Department
Organization
Identifiers
NPS Report Number
NPS-67-82-001CR
Sponsors
The work presented in this report is in support of solid fuel ramj.e
t
research sponsored by Defense Advanced Research Projects Agency (DARPA).
Inother goal of the research is to explore Navy Applications for Advanced
Indirect Fire Support, AIFS
Funding
The AIFS project is also funded by DARPA.
Format
Citation
Distribution Statement
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.