Summary. ESPA 6U Mount (SUM) overview SUM qualification status Future SUM enhancements Moog CSA adapters and ESPA family
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1 Summary ESPA 6U Mount (SUM) overview SUM qualification status Future SUM enhancements Moog CSA adapters and ESPA family 1 CubeSat Summer Workshop 11 August 2012
2 ESPA Six-U Mount SUM Adapter with ESPA standard interface for CubeSat launch Compatible with standard ESPA port interface, Athena II Rideshare Adapter, CubeStack, Atlas V Aft Bulkhead Carrier Prototype developed 2009 Mounts two PPODs or one 6U dispenser Inboard or outboard mounting on ESPA port Inboard mount shares port with exterior mounted ESPA-sat Enables increased capacity for ESPA Six 400-lb satellites and twelve 3U satellites Prototype SUM with one PPOD 2 CubeSat Summer Workshop 11 August 2012
3 ESPA SUM Status Stiffness driven design complete 1 st mode at 150 Hz to minimize launch dynamics Predictions with maximum weight CubeSats August 3 Critical Design Review Manufacturing in progress Qualification program for NASA Launch Services Program Environment requirements for ESPA payloads defined in Rideshare User s Guide (RUG) Testing in October 3 CubeSat Summer Workshop 11 August 2012
4 ESPA Inboard and Outboard Mounting SUM mounts CubeSats internally or externally on ESPA Inboard configuration utilizes ESPA interior Outboard configuration mounts to port OUTBOARD MOUNT 28.3 lbs INBOARD MOUNT 29.0 lbs 4 CubeSat Summer Workshop 11 August 2012
5 SUM with CubeSat Dispensers PSC 6U Dispenser Cal Poly PPODs INBOARD MOUNT OUTBOARD MOUNT 5 CubeSat Summer Workshop 11 August 2012
6 Dispensers Mounted in ESPA with SUM PSC 6U Dispenser Inboard mounting Cal Poly PPODs Outboard mounting 6 CubeSat Summer Workshop 11 August 2012
7 Inboard Configuration Vibration Modes First structural mode for inboard configuration is 159 Hz Mode shape deformations are greatly exaggerated Mode 1: 159 Hz Mode 2: 171 Hz Mode 3: 257 Hz 7 CubeSat Summer Workshop 11 August 2012
8 Outboard Configuration Vibration Modes First structural mode for outboard configuration is 205 Hz Mode shape deformations are greatly exaggerated Mode 1: 205 Hz Mode 2: 206 Hz Mode 3: 318 Hz 8 CubeSat Summer Workshop 11 August 2012
9 Strength Analysis Analysis performed with maximum weight CubeSat simulators inside PPOD models Static analysis with ESPA Rideshare User s Guide (RUG) quasi-static load factors 8.5g in thrust axis and 8.5g lateral No-test factor of safety = 2.0 Random vibration analysis with RUG maximum predicted environment + 3 db (16.2 grms) Crest factor of 3.0 applied to stress RMS levels to predict peak Von Mises stresses 2% critical damping used for analysis Test safety factors: FS y =1.25; FS u = 1.4 All stress margins positive due to RUG loads PPOD configuration allows bending of baseplate 6U dispenser stiffens SUM in this region 9 CubeSat Summer Workshop 11 August 2012
10 RUG Static Loads Analysis Two static load environments applied to SUM with two P-PODs -8.5g in Y direction and 8.5g in Z direction -8.5g in Y direction and 8.5g in X direction Body loads applied in Nastran GRAV feature with appropriate scale factors Y Z X 10 CubeSat Summer Workshop 11 August 2012
11 RUG Random Vibration Protoflight Profile Vibration spectrum for analysis and demonstration test 11 CubeSat Summer Workshop 11 August 2012
12 Planned SUM Enhancements ESPA 24 port version, 12U capability Compatibility with NASA Ames and NASA GSFC/Wallops dispensers SoftRide interface for loads mitigation 12 CubeSat Summer Workshop 11 August 2012
13 Moog CSA Payload Adapters ESPA Flat Adapter CASPAR CubeStack LCROSS ESPA DSX ESPA ESPA as Bus: LCROSS ESPA Grande 42 SepESPA Saab ESPA Variations ESPA with secondary payloads and propulsion system 13 CubeSat Summer Workshop 11 August 2012
14 CubeSat Deployment Sequencer Prototype at Moog Small Satellite exhibit In progress Moog IRAD multi-payload sequencer Modular architecture Compatible with PPOD, PSC, SNC, RUAG systems Circuit and code development Battery testing Moog IRAD multi-payload sequencer Prototype at Moog Small Modular architecture Compatible with PPOD, PSC, Next Primary Vehicle Trigger/Kick Drive 1 Drive 2 Test Ground Interface Table Load Reset Power Power On/Off Release Sequencer SPG 14 CubeSat Summer Workshop 11 August 2012 Drive 3 Drive 4 Drive 5 Drive 6 Drive 7 Drive 8 ESPA Ring
15 Athena Commercial Rideshare Athena IIc annual launches for small satellites STPSat3 Feasibility Assessment completed for DoD Space Test Program Moog CSA payload accommodations Modular multi-payload adapter 4-9 rideshare satellites, kg spacecraft Options for CubeSats and heavier spacecraft SoftRide isolation of adapter and payloads Reduced launch environments Vehicle has similar dynamics with various payload stacks Coupled loads analysis for environment predictions Athena Rideshare Users Meeting 10am Monday Aug 13 Eccles Science Learning Center RM CubeSat Summer Workshop 11 August 2012
16 CubeStack CubeSat adapter by LoadPath and Moog CSA AFRL Space Vehicles Directorate contract Satellites in 10-inch wafer between payload interface and primary Primary interfaces at 24 and 38.8 inches Eight 3U dispensers or combinations of 3U and 6Us Qualification program complete Flight units available Two flight structures ready for delivery Manifested on ORS 3 launch 3 rd quarter 2013 Second generation CubeStack design Bulkhead configuration eliminates lower deck Weight reduced by 15%-20% Improved access for integration CubeStack propulsion module 8-PPOD configuration 16 CubeSat Summer Workshop 11 August 2012
17 Conclusion SUM is one of several new adapters developed for or compatible with CubeSats SUM Critical Design Review complete, proceeding into manufacturing SUM flight units available CubeSat Summer Workshop 11 August 2012
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