1. RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW Boom PER 30 June 2010 113 RBSP EFW Spin Plane Booms Greg Dalton Space Sciences Laboratory University of California, Berkeley

2. RBSP/EFW Boom PER 30 June 2010Greg Dalton 114 SPB Overview SENSOR SPHERE PREAMPLIFIER ENCLOSURE COMPOSITE CABLE FINE WIRE RELEASE MECHANISM METERING WHEEL OVER TENSION HARNESS CONNECTORS SPOOLENABLE PLUG

3. RBSP/EFW Boom PER 30 June 2010Greg Dalton 115 SPB Status F1 & F2 SPB’s ready for cable integration

4. RBSP/EFW Boom PER 30 June 2010Greg Dalton 116 Assembly and Test Flow

5. RBSP/EFW Boom PER 30 June 2010Greg Dalton 117 Facilities and MGSE High Bay deployment for self-shock and length calibration –Door opening self-shock test –Verify proper opening of doors, IDPU indication –Monitor current and voltages of motor, pin puller –Length Calibration, meter wheel turns counter Functional deploy MGSE High Bay flying pulley MGSE

6. RBSP/EFW Boom PER 30 June 2010Greg Dalton 118 Facilities and MGSE Vibration Facility – Quanta Laboratories, Santa Clara –Readily available for testing –Force limiting test performed on ETU –One instrument per day Vibration per EDTRD: Vibe fixtures for RBSP S/C mounting – force limiting Unpowered Testing ETU to qualification levels, flight to protoflight levels Test sequence on all three axis: o Fixture only all tests o ¼ G sweep to verify 1 st mode o ½ G @ 40 Hz to validate controller and force gages o Random o ¼ G Sweep o 5-100 Hz Sine Strength o ¼ G Post Sweep

7. RBSP/EFW Boom PER 30 June 2010Greg Dalton 119 Facilities and MGSE Thermal Vacuum Chamber – SSL –Chamber used on for THEMIS SPB deployments –Mechanical GSE ready for TVAC deployment –Chamber prepared for testing

8. RBSP/EFW Boom PER 30 June 2010Greg Dalton 120 Facilities and MGSE Deployment Sequence (video)

9. RBSP/EFW Boom PER 30 June 2010Greg Dalton 121 TVAC Profile One full survival cycle 3 operational temperature cycles Hot deploy Cold Deploy Six cycles total CPT to verify electronics functionality

10. RBSP/EFW Boom PER 30 June 2010Greg Dalton 122 ECN Summary ECN-006 –ECN closed out –New Parts made, added to Cable Fabrication assembly –Description:

11. RBSP/EFW Boom PER 30 June 2010Greg Dalton 123 RFA Summary EFW-CDR-10/11 –RFA from CDR closed out –Analysis was completed and report delivered –Description: EFW-CDR-10 Action: Verify deployment ring spring stress margin (update stress table on chart 466) Increasing spring tension lowers stress margin. Rationale: Deployment ring uses two springs in tension to help actuate the restraint mechanism. EFW-CDR-11 Action: Verify deployment spring force margin at worst case condition Rationale: Deployment ring uses two springs in tension to help actuate the restraint mechanism.

12. RBSP/EFW Boom PER 30 June 2010Greg Dalton 124 PFR Summary PFR-006 –PFR dated 4/7/10 closed out –PFR report submitted and accepted –Description: While removing SPB Preamplifier PWB Assembly #16 from the Preamplifier TVAC MGSE, the Ferrule Spring caught on the technicians glove and was pulled from the Preamplifier Enclosure. The technician bobbled the PWB Assembly, which then rolled down the technician's smock, along the technician's pant leg to his shoe, then free-fell a distance of 6 inches to the floor. –Corrective Action/Resolution: The SPB #16 Preamplifier PWB Assembly was inspected under a microscope by SSL QA. It was then electrically bench tested satisfactorily, then satisfactorily completed a thermal vacuum electrical test.The corrective action is to take care when handling Preamplifier PWB Assemblies, ensuring the preamplifier is assembled/disassembled near a surface and removes the possibility of dropping. The technician shall use a pair of tweezers to remove the Preamplifier PWB Assembly and maintain positive control. This will minimize the risk of the Ferrule Spring from catching on gloves, ESD jacket sleeve, or other GSE.

13. RBSP/EFW Boom PER 30 June 2010Greg Dalton 125 SPB Status Instrument Status –F1 instruments are completely built, CPT complete, initial High Bay deployment (self-shock) and length calibration complete –F2 instruments at built at sub-component level –Flight Spares (2) are built at sub-component level –All instruments built to print per RBSP-EFW-SPB-003 Indentured Drawing List Revision C Documentation –Travelers complied –No outstanding ECN’s, RFA’s, or PFR’s –Procedures for environmental testing are signed off Electrical Comprehensive Performance Test Vibration Test Procedure Thermal Vacuum Test Procedure

14. RBSP/EFW Boom PER 30 June 2010Greg Dalton –This page intentionally almost blank 126