Northrop Grumman — Fact Sheet (2018)

2 slides from Northrop Grumman's fact sheet, 2018

Slide 1: GMLRS IM Rocket Motor
GMLRS® IM Rocket Motor N orthrop Grumman developed a new, advanced Guided Multiple Launch Rocket System (GMLRS) rocket motor that meets current flight requirements and stringent insensitive munitions (IM) requirements while adding an increased level of safety Product Features and Benefits • • • IM p
Slide 2: Specifications
Specifications Technical Data Weight: 340 lb (154.2 kg) total Length: 88.6 in (2199.6 mm) max Diameter: 9.1 in (231.1 mm) max Case: Graphite/Kevlar® composite Temperature: -26°F to +140°F (-32°C to +60°C) Insulator: R181 aramid-filled ethylene propylene diene monomer (EPDM) Propellant: Aluminized hy