Design and Implementation of a Thrust Vector Control (TVC) Test System
Öz
The rocket engines are tested statically to evaluate
the performance of engine based upon thrust produced. One of the most important
parameters of the rocket engine static testing evaluation is to measure the
thrust produced by the engine. The thrust produced is measured using a Thrust Vector
Control (TVC) test system which is a structural element equipped with load
cells. In this study, a load sensor system was designed to measure the
propulsion performance of a solid propellant rocket motor. The forces and
moments of the rocket motor with respect to the six degrees of freedom of the
test system were measured during firing. It is seen that the obtained
experimental results and the analysis results are compatible with each other.
The designed stand is capable of measuring axial thrust and lateral
(misaligned) thrust components, and the rolling moment for rocket motors
producing axial thrust up to 50 [kN].
Anahtar Kelimeler
Kaynakça
- [1] Runyan R.B., Rynd J.P., Seely J.F., “Thrust stand design principles”, AIAA 17th Aerospace Ground Testing Conference, July 6-8, Nashville, TN, USA, (1992).
- [2] Turner M.J.L., Rocket and spacecraft propulsion. Principles, Practice and new development (Third edition), Springer-Praxis Publishing Co., U.K, (2009).
- [3] Mattingly J.D., Elements of propulsion: Gas turbines and rockets, AIAA Publishing Inc., Virginia, USA, (2006).
- [4] Brimhall Z.N., Atkinson J.P., Kirk D.R., Peebles H.G., “Design of a novel six degree of freedom solid rocket motor test stand”, AIAA 2007-5331 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 8-11, Cincinnati, OHI, USA, (2007).
- [5] Brimhall Z.N., Divitotawela N., Atkinson J.P., Kirk D.R., Peebles H.G., “Design of a novel six degree of freedom solid rocket motor test stand”, AIAA 2007-5331 44th IAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 21-23, Hartford, CT, USA, (2008).
- [6] Gligorijevic N., Zivkovic S., Subotic S., Kozomara S., Nikolic M., Citakovic S., “Side force determination in the rocket motor thrust vector control system”, Scientific Technical Review, 63(1): 27-38, (2013).
- [7] Wekerle T., Barbosa E.G., Batagini C.M., Costa L.E.V.L., Trabasso L.G., “Closed-loop actuator identification for Brazilian Thrust Vector Control development”, IFAC-PapersOnLine, 49(17): 468–473, (2016).
- [8] Milos P., Davidovic N., Jojic B., Milos M., Todic I., “A novel 6 DOF thrust vector control test stand”, Tehnicki Vjesnik-Technical Gazette, 22(5): 1247-1254, (2015).
Ayrıntılar
Birincil Dil
İngilizce
Konular
Mühendislik
Bölüm
Araştırma Makalesi
Yayımlanma Tarihi
1 Haziran 2018
Gönderilme Tarihi
25 Ocak 2018
Kabul Tarihi
-
Yayımlandığı Sayı
Yıl 2018 Cilt: 21 Sayı: 2
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