MPSRReaction Control System 1 UCB, 26 October 2006 THEMIS PROBE MISSION PRE-SHIP REVIEW (Update on repressurization) Michael Sholl University of California.

Slides:



Advertisements
Similar presentations
DOC-TAS-EN-002 ExoMars-2018 DM Entry Decent Landing LSSWS# December 2014 Turin.
Advertisements

Technologies for Low Cost Reusable Launch Vehicles Eric Besnard, Professor California State University, Long Beach (562)
MPSRESA- 1 UCB, Oct 26, 2006 THEMIS MISSION PRE-SHIP REVIEW ESA C. Carlson, M. Ludlam, J. McFadden University of California - Berkeley.
Babakin Space Center, Space Research Insitute, Makeev Rocket Design Bureau COSMOS ONE: THE FIRST SOLAR SAIL a project of The Planetary Society with Cosmos.
AAE450 Spring 2009 Descent Trajectory Hover Trajectory LD Code Integration John Aitchison March 5 th, 2009 [John Aitchison] [Mission Ops]
28 October st Space Glasgow Research Conference, Glasgow, United Kingdom.
MPSRThermal- 1 UCB, Oct 26, 2006 THEMIS MISSION PRE-SHIP REVIEW Thermal Christopher Smith University of California - Berkeley.
THEMIS INSTRUMENT PER 1 UCB, May, 2005 EMC / Mag Instrument Test Plan & Results Michael Ludlam University of California - Berkeley.
1 UCB, May 04, 2005 Magnetometer Booms Vibration Issues Berkeley Composites Laboratory Department of Mechanical Engineering University of California at.
The Boeing 777 can hold a max of 550 passengers on board and 2 crew members.
MPSRReaction Control System 1 UCB, 26 October 2006 THEMIS PROBE MISSION PRE-SHIP REVIEW Reaction Control System Michael Sholl University of California.
Ryan Mayes Duarte Ho Jason Laing Bryan Giglio. Requirements  Overall: Launch 10,000 mt of cargo (including crew vehicle) per year Work with a $5M fixed.
THEMIS SRR Requirement Overview - 1 UCB, 07/08/2003 REQUIREMENT DEVELOPMENT OVERVIEW Ellen R. Taylor Mission Systems Engineer Space Science Laboratory.
THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley.
MPSREFI- 1 UCB, Oct 26, 2006 THEMIS MISSION PRE-SHIP REVIEW “Our Gateway to the Cape…” The Electric Field Instrument (EFI) John Bonnell University of California.
MPEREMC 1 UCB, June 23, 2006 THEMIS MISSION PRE-ENVIRONMENTAL REVIEW Probe 2 EMC Test Results David Curtis University of California - Berkeley.
Upper Stage Weekly Summary 3/3 – 3/9/2008 Talked to Joe about simulation Joe said that the Δv’s seemed high but reasonable Joe suggested running simulations.
THEMIS peer Instrument CDR 1 CETP, Paris, April 8, 2004 THEMIS Mission Status at Peer UCB Instrument Critical Design Review UCB, April 19/20, 2004 Vassilis.
LAT-TD GLAST LAT Project Tracker Inner Shipping Container Analysis and Test Results Tracker Inner Shipping Container Analysis and Test Results August.
MPSRAlignments - 1 UCB, Oct 26, 2006 THEMIS PROBE MISSION PRE-SHIP REVIEW Alignments Paul Turin LME University of California - Berkeley.
THEMIS FGM CDR Peer ReviewBerlin, April 6, 2004 THEMIS FGM Engineering Peer Review SC Integration and Test Ellen Taylor University of California - Berkeley.
Competition Sensitive Dennis Asato June 28, 2001 XSuperNova / Acceleration Probe (SNAP) Propulsion.
Polar Gateways 2008THEMIS Constellation Operations − Jan 2008 THEMIS Constellation Operations Dr. Manfred Bester University of California at Berkeley.
THEMIS PER 1 UCB, May 02, 2005 Magnetometer Booms Pre Environmental Review Prof. Hari Dharan Berkeley Composites Laboratory (Presenter: David Pankow) Department.
MPSRQA- 1 UCB, Oct 26, 2006 THEMIS MISSION PRE-SHIP REVIEW Mission Assurance Manager Ron Jackson University of California - Berkeley.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW I-PER 21 January EFW Overview and Status Keith Goetz University of Minnesota.
15-16 June THEMIS Propellant Offload Concept M. Sholl (UCB) M. McCoullough (SAI) P. Turin (UCB) June 2005 MIWG/GOWG(TIM) Space Sciences Laboratory.
Max-Planck- Institut für Plasmaphysik Karsten Liesenberg / AS-T Visit NCSX engineers 11/12 October 2007 Final assembly of Stellarator W7-X in the torus-assembly.
THEMIS IDPU PDR I&T REQUIREMENTS- 1 UCB, October 16, 2003 I&T REQUIREMENTS Ellen Taylor University of California - Berkeley.
Energy and Work Energy and Its Conservation Chapters 10 & 11.
Precision Measurement Fundacións of Engineering and Technology.
THEMIS FDMO Review Propellant Budget Update − 1 October 5, 2004 PROPELLANT BUDGET UPDATE Vassilis Angelopoulos Covered in this presentation: Allocations.
FM2 PPSRRCS Pressure Test Leak Check 1 UCB, March 16, 2006 THEMIS PROBE FM2 PRE-ENVIRONMENTAL REVIEW RCS MEOP TEST/LEAK CHECK Michael Sholl Berkeley RCS.
SWT Overview 1 UCB, Nov15/16, 2006 THEMIS SCIENCE WORKING TEAM MEETING Mission Overview Peter R. Harvey Project Manager University of California - Berkeley.
Bounds Bingo!. Pick any 9 of these numbers
FM1 Instrument Suite Pre-Ship Review (PSR)INT- 1 UCB September 21, 2005 THEMIS FM1 INSTRUMENT SUITE PRE-SHIP REVIEW (PSR) INTEGRATION AND TEST PLANS Jeremy.
FM2 PPEREMC 1 UCB, March 16, 2006 THEMIS PROBE FM2 PRE-ENVIRONMENTAL REVIEW EMC Test Dave Curtis System Engineer University of California - Berkeley.
FM2/FM3 PSR FM4/FM5 PERSCM - 1UCB, November 10, 2005 THEMIS FM2/FM3 INSTRUMENT SUITE PRE-SHIP REVIEW (PSR) THEMIS FM4/FM5 INSTRUMENT SUITE PRE- ENVIRONMENTAL.
THEMIS Instrument PDRMission Assurance- 1 UCB, October 15-16, 2003 THEMIS Mission Assurance Preliminary Design Review Ron Jackson University of California.
Open up your notes at page 15, note 24, Newton’s Laws and Space Travel. Work in pairs - Attempt to fill in the blank space in note 24. weight W = ? m =
1 EstimationStrategies Press Ctrl-A ©2009 – Not to be sold/Free to use Stage 5 Year 9.
THEMIS Instrument CDR 1 UCB, April 19-20, 2004 EFI Preamp Sensor G.T. Delory, A. Hull, D. Schickele, J. Bonnell & The EFI Team University of California.
Friction and Forces on Inclined Planes. The Normal Force The normal force is the supporting force that acts on the object perpendicular to the surface.
THEMIS MRRSystems - 1 GSFC, Jan 5, 2007 Systems Engineering.
FM1 Instrument Suite Pre-Ship Review (PSR)AGENDA 1 UCB, September 21, 2005 THEMIS T IME H ISTORY OF E VENTS AND M ACROSCALE I NTERACTIONS DURING S UBSTORMS.
Launch Structure Challenge - Background Humans landed on the moon in 1969 – Apollo 11 space flight. In 2003, NASA started a new program (Ares) to send.
THEMIS Critical Design Review Reaction Control Subsystem
FM4/FM5 IPSRSYS - 1 UCB, May 5, 2006 THEMIS INSTRUMENT SUITE FM4/FM5 PRE-SHIP REVIEW SYSTEM OVERVIEW Ellen Taylor University of California - Berkeley.
Engineering Analysis & Updated Layout Drawings SofaKing 9 March 2005.
PIT – What it is PIT - Pulsed Inductive Thruster NuPIT – Nuclear Pulsed Inductive Plasma Step after the grided ion thruster Advantage: No Electrode –No.
MISSION PRE-ENVIRONMENTAL REVIEW
THEMIS MISSION PRE-SHIP REVIEW
THEMIS Mission Confirmation Readiness
MISSION PRE-ENVIRONMENTAL REVIEW
continued on next slide
THEMIS MISSION PRE-SHIP REVIEW
                                                                                                                                                                                                                                                
continued on next slide
continued on next slide
Bounds Bingo!.
Sugar Brick: Charcoal Briquette Compactor
PRIME Ki-systems update
Title Presentation PPT submission deadline: 31 August, 2019 Speaker:
© T Madas.
Year 8 Answers to Data Handing Challenge
(a) Find the PE at A PE = m g h = ( 500 kg )( 9.8 m/s2 )( 30 m )
continued on next slide
STRUCTURES & WEIGHTS QDR 1
Propulsion Jon Lewis Mike Rhee 8/19/99
continued on next slide
Presentation transcript:

MPSRReaction Control System 1 UCB, 26 October 2006 THEMIS PROBE MISSION PRE-SHIP REVIEW (Update on repressurization) Michael Sholl University of California – Berkeley RCS Engineer

MPSRReaction Control System 2 UCB, 26 October 2006 Repressurization Limits Thruster qualification levels (MR111C 1lbf thrusters) Steady-state upper limit: 450psi Pulsed upper limit: 400psi (Radarsat, Landsat 6) THEMIS operational upper limit: 400psi Pulsed qualification lower limit: 80psi Additional ATP testing on all THEMIS flight units to 50psi THEMIS operational lower limit: 75psi Required: Offload 0.5kg N 2 H 4 ( see next slide )

MPSRReaction Control System 3 UCB, 26 October 2006 Operational Constraints 10m/s Δν required by mission operations (0.5kg) N 2 H 4 loading requirement: 48.8kg ±0.2kg KSC fueling group scale accuracy: 0.2kg Precision weights used to increase accuracy further Conclusion: healthy repressurization margins with 0.5kg N 2 H 4 offload