產品介紹∣實驗室等級火箭發動機

特點
Features

實驗室規模測試火箭發動機 LTRM™ 用作 SV-2 (Stojan Vessel®) 的輔助設備，或作為在小規模實驗室條件下測定固體火箭推進劑燃燒速率的低成本解決方案。
可以使用 EDA 或 EDAL 高速分析儀在 LTRM 上測量壓力-時間燃燒曲線。

應用

建議將 LTRM 與 Stojan 高壓釜試驗儀結合使用，特別是用於新成份、催化劑和添加劑的研究與開發，或用於製造固體火箭推進劑的品質控制及其在役監控。

在 SV-2 或 SSB 試驗結果的基礎上，LTRM 試驗提供了更多的附加資訊（最大和平均壓力值、壓力脈衝、燃燒時間、固體火箭推進劑燃燒率、特徵速度、溫度敏感係數等）。其測試效果接近全尺寸火箭發動機的成本效益。

ABSW 軟體畫面

優勢和特點

僅測量壓力 – 不具推力！
工作壓力最高達 500 bar。
具有兩個過壓保護裝置，安全等級高。
操作簡單。
與Stojan高壓釜試驗儀SV-2 或 EDA 分析儀結合使用效果更佳。
不銹鋼支架上有一個籠子，用於收集燃燒後的微顆粒。
包括測試發動機和用於評估的 ABSW™ 軟體。

合規

STANAG 4672
STANAG 4673

LTRM 結構

The Lab-Scale Testing Rocket Motor LTRM™ is used as an auxiliary equipment to the SV-2 (Stojan Vessel®) or as a low-cost solution for the determination of burning rate of solid rocket propellants in sub-scale laboratory conditions. Pressure-time burning profiles can be measured on LTRM using EDA or EDAL high-speed analyzers.

APPLICATIONS
Combination of LTRM with Stojan Vessel is recommended especially for research and development of new compositions, catalysts and additives or for quality control of manufactured solid rocket propellants and their in-service surveillance.

Testing by LTRM provides more additional information to results obtained by SV-2 or SSB tests (values of maximal and mean pressure, impulse of pressure, burning time, burning rate of solid rocket propellant, characteristic velocity, temperature sensitivity coefficient, etc.). These results are close to the full-scale rocket motor in a cost effective way.

ABSW software screenshot

ADVANTAGES & FEATURES

Only pressure measurement - No thrust!
Working pressure up to 500 bar
High level of safety with two overpressure protections
Simple operation
Beneficially combined with Stojan Vessel SV-2 or EDA analyzer
Stainless steel stand with a basket for catching small burning particles
Testing motor and the ABSW™ sofware for evaluation included

COMPLIANCE

STANAG 4672
STANAG 4673

LTRM detail