Lazansky C-Refinement of a Low-Shock Separation System- 41st Aerospace Mechanisms Symposium, Jet Propulsion Laboratory2012.
Lazansky C-Refinement of a Low-Shock Separation System- 41st Aerospace Mechanisms Symposium, Jet Propulsion Laboratory2012.
Rudoy E, inventor; G & H Technology, Inc., assignee-Non-Explosive Separation Nut1993.
Rudoy E, inventor; G & H Technology, Inc., assignee-Non-Explosive Separation Nut1993.
Chaput DT, inventor; G & H Technology, Inc., assignee-Separation Nut With a Restraining Wire1994.
Chaput DT, inventor; G & H Technology, Inc., assignee-Separation Nut With a Restraining Wire1994.
William D-Nygren J, inventor; Martin Marietta Corp., assignee-Flywheel Nut Separable Connector and Method1997.
William D-Nygren J, inventor; Martin Marietta Corp., assignee-Flywheel Nut Separable Connector and Method1997.
Smith SH, inventor; Saab Ericsson Space AB, assignee-Device and Method for Connecting Two Parts of a Craft2002.
Smith SH, inventor; Saab Ericsson Space AB, assignee-Device and Method for Connecting Two Parts of a Craft2002.
Thenander M, inventor; Ruag Space AB assignee-Separable Roller Screw Assembly for a Space Craft Release Mechanism System2020.
Thenander M, inventor; Ruag Space AB assignee-Separable Roller Screw Assembly for a Space Craft Release Mechanism System2020.
Rao BN JD, Biswas KK-Rigid Body Separation Dynamics for Space Launch Vehicles-Aeronaut J-2006. [
DOI:10.1017/S0001924000013166]
Rao BN JD, Biswas KK-Rigid Body Separation Dynamics for Space Launch Vehicles-Aeronaut J-2006. [
DOI:10.1017/S0001924000013166]
Jeyakumar D RB-Dynamics of Satellite Separation System-J Sound Vib-2006. [
DOI:10.1016/j.jsv.2006.03.035]
Jeyakumar D RB-Dynamics of Satellite Separation System-J Sound Vib-2006. [
DOI:10.1016/j.jsv.2006.03.035]
Singaravelu J JDaRB-Reliability and Safety Assessments of The Satellite Separation Process of a Typical Launch Vehicle-J Defense Model Simul: Appl Method Technol-2012.
Singaravelu J JDaRB-Reliability and Safety Assessments of The Satellite Separation Process of a Typical Launch Vehicle-J Defense Model Simul: Appl Method Technol-2012.
Hu XZ CX, Tuo ZH-Dynamics And Transient Perturbation Analysis Of Satellite Separation Systems-Proc IMechE, Part G: J Aerospace Engineering-2012. [
DOI:10.1177/0954410012466780]
Hu XZ CX, Tuo ZH-Dynamics And Transient Perturbation Analysis Of Satellite Separation Systems-Proc IMechE, Part G: J Aerospace Engineering-2012. [
DOI:10.1177/0954410012466780]
SZ TXaY-Dynamic Simulation and Failure Analysis of a Clamp Band System for Spacecraft-J Tsinghua University (Sci Tech)-2010.
SZ TXaY-Dynamic Simulation and Failure Analysis of a Clamp Band System for Spacecraft-J Tsinghua University (Sci Tech)-2010.
Li JL YSaTX-Dynamic-Envelope Analysis of Clamp-Band Joint Considering Pryroshock of Satellite Separation-J Spacecr Rockets-2014. [
DOI:10.2514/1.A32382]
Li JL YSaTX-Dynamic-Envelope Analysis of Clamp-Band Joint Considering Pryroshock of Satellite Separation-J Spacecr Rockets-2014. [
DOI:10.2514/1.A32382]
KY C-V-Band Separation Shock Characteristics-75th Shock and Vibration Symposium, Virginia ,Beach-2004.
KY C-V-Band Separation Shock Characteristics-75th Shock and Vibration Symposium, Virginia ,Beach-2004.
Han X JAaWR-Shock Tests for Low Shock Device of Wrapping Band and Related Data Processing-Spacecr Environ Eng-2007.
Han X JAaWR-Shock Tests for Low Shock Device of Wrapping Band and Related Data Processing-Spacecr Environ Eng-2007.
Lancho M GE, Rivas J-LPSS: a Clamp Band Release System Inducing Low Shock at Payload Interface-57th International Astronautical Congress-2006. [
DOI:10.2514/6.IAC-06-C2.7.07]
Lancho M GE, Rivas J-LPSS: a Clamp Band Release System Inducing Low Shock at Payload Interface-57th International Astronautical Congress-2006. [
DOI:10.2514/6.IAC-06-C2.7.07]
David Dowen SC, Andrew Peffer-Development of a Reusable, Low-Shock Clamp Band Separation System for Small Spacecraft Release Applications- 15th Annual/USU Conference on Small Satellites.
David Dowen SC, Andrew Peffer-Development of a Reusable, Low-Shock Clamp Band Separation System for Small Spacecraft Release Applications- 15th Annual/USU Conference on Small Satellites.
Bhosale R RVaSS-Motion Analysis of Band Release System-Int J Eng Res Dev-2012.
Bhosale R RVaSS-Motion Analysis of Band Release System-Int J Eng Res Dev-2012.
Arun Thampi ARAK-Joint Characteristic Study of a Typical Merman Band Joint Used for Launch Vehicles Using Non-Linear Fe Analysis-International Journal of Engineering Research & Technology-2014;03(07).
Arun Thampi ARAK-Joint Characteristic Study of a Typical Merman Band Joint Used for Launch Vehicles Using Non-Linear Fe Analysis-International Journal of Engineering Research & Technology-2014;03(07).
Juho Lee D-HH, Jae-Kyeong Jang, Dong-Jin Kim, YeungJo Lee, Jung-Ryul Lee, and Jae-Hung Han-Pyroshock Prediction of Ridge-Cut Explosive Bolts Using Hydrocodes-Shock and Vibration-2016. [
DOI:10.1155/2016/1218767]
Juho Lee D-HH, Jae-Kyeong Jang, Dong-Jin Kim, YeungJo Lee, Jung-Ryul Lee, and Jae-Hung Han-Pyroshock Prediction of Ridge-Cut Explosive Bolts Using Hydrocodes-Shock and Vibration-2016. [
DOI:10.1155/2016/1218767]
Shihui Xiong YY, Yanhua Li , and Yuquan Wen-Numerical Study on the Explosive Separation of Pyrotechnic Cutter-Shock and Vibration-2019. [
DOI:10.1155/2019/2457854]
Shihui Xiong YY, Yanhua Li , and Yuquan Wen-Numerical Study on the Explosive Separation of Pyrotechnic Cutter-Shock and Vibration-2019. [
DOI:10.1155/2019/2457854]
Alberto Sanchez Cebrian B-UHaTG-RUAG's Approach to Develop a Modular Low Shock Separation and Jettison System- 8TH European Conference for Aeronautics and Space Sciences; Madrid, Spain2019.
Alberto Sanchez Cebrian B-UHaTG-RUAG's Approach to Develop a Modular Low Shock Separation and Jettison System- 8TH European Conference for Aeronautics and Space Sciences; Madrid, Spain2019.
Xueting Pan YZ, Yifan Lu, Fei Yang & Honghao Yue-A Reusable SMA Actuated Non-Explosive Lockrelease Mechanism for Space Application-International Journal of Smart and Nano Materials-2020.
Xueting Pan YZ, Yifan Lu, Fei Yang & Honghao Yue-A Reusable SMA Actuated Non-Explosive Lockrelease Mechanism for Space Application-International Journal of Smart and Nano Materials-2020.
امین طلائی زاده، منصور کبگانیان، مرتضی شهروی-تحلیل دینامیکی فرآیند جدایش سامانه کاهش مدار یک سفینه بازگشت پذیر- سیزدهمین کنفرانس انجمن هوافضای ایران; تهران، دانشگاه تهران1392.
امین طلائی زاده، منصور کبگانیان، مرتضی شهروی-تحلیل دینامیکی فرآیند جدایش سامانه کاهش مدار یک سفینه بازگشت پذیر- سیزدهمین کنفرانس انجمن هوافضای ایران; تهران، دانشگاه تهران1392.
محمد جواد اسکندری، علیرضا نوین زاده، رضا میرزایی، یاسر زروندی-تحلیل و شبیه سازی شش درجه آزادی دینامیک سیستم جدایش فنری ماهواره ها و موشک های چند مرحله ای- اولین همایش یافتههای نوین در هوافضا و علوم وابسته; تهران، دانشگاه تهران1394.
محمد جواد اسکندری، علیرضا نوین زاده، رضا میرزایی، یاسر زروندی-تحلیل و شبیه سازی شش درجه آزادی دینامیک سیستم جدایش فنری ماهواره ها و موشک های چند مرحله ای- اولین همایش یافتههای نوین در هوافضا و علوم وابسته; تهران، دانشگاه تهران1394.
A.S-Pouzada ECF, A.J-Pontes-Friction Properties of Moulding Thermoplastics-Department of Polymer Engineering, IPC/Institute for Polymers and Composites, University of Minho, Portugal-2006. [
DOI:10.1016/j.polymertesting.2006.06.009]
A.S-Pouzada ECF, A.J-Pontes-Friction Properties of Moulding Thermoplastics-Department of Polymer Engineering, IPC/Institute for Polymers and Composites, University of Minho, Portugal-2006. [
DOI:10.1016/j.polymertesting.2006.06.009]
