Advanced Solid Fuel Ramjet Demonstrator Coalition Warfare Program

reportActive / Technical Report | Accession Number: AD1102496 | Open PDF

Abstract:

Project Motivation Long Range Propulsion - Density specific impulse is an indicator of range potential for propulsion systems Thrust per fuel mass flow rate SFRJ have greatest range potential. Solid metalized fuels have higher energy density than liquids JP 10 SFRJ are mechanically simple and can readily be scaled over tactical sizes Recent 3.0 flight demonstrated at NAWCWD.

Author(s):
Hedman, Trevor
Author Organization(s):
Naval Air Warfare Center Weapons Division China Lake United States
Descriptive Note:
Conference Paper
Supplementary Note:
Pacific Operational Science and Technology (POST) Conference 2018, 05 Mar 2018, 09 Mar 2018,
Pagination:
0014

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release;

RECORD

Collection: TR
Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Communities of Interest:
Weapons Technologies
Descriptor(s):
propulsion systems, rocket engines, solid fuels, combustion, trajectories, thrust, high energy, surface launched
Field(s)/Group(s):
Surface Transportation and Equipment, Rocket Engines
Keyword(s):
Pacific Operational Science and Technology (POST) Conference, 2018, POST 2018, PACOM, USPACOM, USINDOPACOM, INDOPACOM, CWP, sfrj, asfrj(Advanced Solid Fuel Ramjet (ASFRJ) demonstrator which), srm(solid rocket motors)
Report Date:
2018 Mar 08
Creation Date:
2020 Jun 25