Savunma Roket Motoru: NFPA 495, Solid Propellant HMX ve NEW Hesabi

Savunma roket motorlari kati yakitli (HMX, HTPB, AP) propellant icerir. Bir Stinger fuze yaklasik 2 kg propellant, HIMARS 90 kg, SM-3 1300 kg. NEW (Net Explosive Weight) ve IMESAFR Quantity Distance uretim tesisi layoutunu belirler. NFPA 495 ve DoD 6055.09 ABAO kurallarini verir.

Propellant Kimyasi

• AP (ammonium perchlorate): 70 percent typical
• HTPB binder: Polimer 12-15 percent
• HMX: Secondary explosive yüksek enerji
• Al tozu: 15 percent performance boost
• Yanma hizi: 5-30 mm/sn tipik

Class 1.1 vs 1.3

• Class 1.1: Mass detonation (HMX/RDX)
• Class 1.3: Mass fire (AP composite)
• Card gap test: Sensitivity olcer
• UN test 6c: Bullet impact
• CBI: Classification Body Investigation

Uretim Hatti Koruma

• Mixing building: Remote, barricaded
• Blast door: 10 bar dayanim
• Deluge: 20.4 L/min/m2 ozel
• Ex elektrik: Zone 1 Group IIB
• Static grounding: 1 ohm

Test ve Depolama

• Static test: Blast wall 45 derece
• Magazine: Earth-covered 3 m toprak
• IBD: K40 siviller
• IMD: K11 magazine-magazine
• Temperature: 25+-5 C stabil

Turk Savunma Sanayii

• Roketsan Elmadag: SOM, Karaok, TRG
• MKE Kirikkale: Muhimmat
• TUBITAK SAGE: Arge tesisi
• Aselsan Akyurt: Guidance kit
• NATO STANAG: Uyumluluk gereksinimleri

Roket SprinkCalc ile

SprinkCalc roket motoru uretim NEW hesabi, deluge 20.4 L/min/m2, IMESAFR K-scaled distance, Zone 1 IIB ve NFPA 495 blast door kontrolu yapar.

SprinkCalc'i App Store'dan indir