# Presentation: 445867

## Section 2

_***Section 2***_
***Observatory Readiness***

*** ******. . . Dale Schulz***
*EO-1 Project Manager*

***Completion of Verification***
***Action Item Status***
***Launch Campaign Status***

## Completion of Verification

## “As Conducted” Final System Level Spacecraft Verification

## Technical Peer Reviews

***Technical Peer Reviews***

***Significant Peer Reviews that occurred prior to March 2000 were presented as Special Topics at the Red Team Review***
***Two Peer Reviews were held prior to the Delta Pre-Ship Review resulting from Red Team RFAs***
***Safehold Test On-Orbit -- Directors of 300, 400, and 500 have concurred with the planned testing on Day 2***
***Additional Vibration Test -- AETD Panel concurred with the Project that the benefit of the test was not worth the risk***
***One Peer Review has been conducted since the Delta Pre-Ship Review -- Review of decisions to defer to system-level testing or delete requirement for box-level testing based on qualification by analysis or by similarity  ***

## EO-1 Verification by Analysis or Similarity

***EO-1 Verification by Analysis or Similarity***

## Launch Campaign Flow

***Launch Campaign Flow***

- * in parallel with SAC-C processing

## TV II Test Profile (7/1 17/00)

- External Stim. Verif. Test (6hrs)
- Roll S/C into T/V chamber(4hrs)
- Functional Test (12 hrs)
- CPT0(4hrs)
- Depress
- CPT 1(4hrs)
- Turn on Hyperion Outgas heaters (GSE)
- Power down (4hrs)

- Power Up (1/2 hr)
- (Prelaunch Aliveness Test)
- (WARP on, ALI radiator htrs on)

- Shroud goes Cold

- Functional Test (12 hrs)(ALI & Hyp to outgas)
- ALI Warm_Period Terminated
- CTV S-band Special Test (2hrs)
- CTV X-band Test  (2hrs)
- Turn off Hyperion Outgas heaters
- All Instrument DCE (AC off) (1 hr)
- MOC Cont Procs (non-inst) (4hrs)
- Power Down (1/4 hr)

- Transition - Powered off

- Transition - Powered off

- Transition - Powered off

- Power Up (1/2 hr)
- Heater Verification (1hr)
- Powerdown
- Functional Test  (12 hr)
- CTV S-band Special Test  (2hrs)
- CTV X-band test (2hrs)
- Powerdown
- CPT 0(4hrs)
- CPT1(5 hrs) (WARP on)
- M5 Stress Test (5 hrs)
- Hyperion ASP Temp Test (2hrs)
- All InstrDCE (1 hr) (AC/Hyp Stim)
- Config for Instrument Turn On Sim
- Instrument Turn on Sim (24 hrs)

- Instrument Turn-on Sim, continued (12hrs)
- MOC Instrument/WARP Proc Checkout (4hrs)
- ALI Decontamination Test (6 hr)
- Hyperion ASP Temperature Test (2hrs)
- M5 Stress Test (5 hrs)
- All Instrument DCE (AC off) (1hr)
- Power Down (1/4 hr)

- CPT Config
-  WARP Power on (Htr proc-1/2hr)
- CPT2 (w/ CTV 10 hrs)
- ACS Special tests (1.5hrs)
- CPT 3 (7 hrs)
- CPT 4F (4hrs)
- CPT 5 (12 hrs)
- CPT 6 (5hrs)
- CPT 7 (3hrs)
- CPT 8 (3hrs)
- AC/Hyperion Cross Cal Test (2 hr)
- CPT 11 (5 hrs)
- CPT 9 (6 hrs)
- CPT 10 (7hrs)
- Power off (0.5 hr)
- 1773 Characterization Test(4hrs)
- Observatory Power On (1/2hr)

- Instrument Contigency Sim (4hrs)
- All Instrument DCE (1hr)
- Power Down
- CPT0(4hrs)
- CPT 1(5hrs) (WARP on)
- CPT2 (With CTV) (10 hrs)
- ACS Special Tests (1.5hrs)
- CPT 3 (7hrs)
- CPT 4F(4hrs)
- CPT 5 (12 hrs)
- CPT 6 (5 hrs)
- CPT 7 (without AC) (3 hrs)
- CPT 8 (without AC) (3 hrs)
- CPT 11 (5 hrs) (Hyp bakeout after DCE)
- CPT 9 (6 hrs)
- CPT 10 (7 hrs)
- 1773 Characterization Test (4hrs)
- Open ALI Aperture Door (in parallel)
- ALI Bakeout (3 hrs)
- Close ALI Aperture Door (1/4 hr)
- Power Down (1/4 hr)

- Repress
- Attach cooling air (1 hr)
- Functional Test (12 hrs)
- ALI latch reset

**0**
**(16hrs)**

**    ****1**
**(8 hrs)**

**2 (6 hrs)**

**3**
**(24 hrs)**

**     ****4   **
**(13 hrs)**

**5**

**6**

**     ****7**
** ****(60 hrs)**
**(5,6,7)**

**11**
**(75 hrs)**

**    ****12**
**(12 hrs)**

**13**
**(80hrs)**

**14**
**(4hrs)**

**15**
**(6hrs)**

- Instrument Turn-on Sim, Continued
- RCS Sec  Htr Test  (1hr)

- Nominal Operations SIM
- (12 hrs)

**9**
**(28 hrs)**

**   ****8**
**(12 hrs)**

**   ****10**
**(6 hrs)**

**16**
**(8 hrs)**

**+40****o****C**

**Ambient**

**+5****o****C**
**  ****0****o****C**

**17**
**(13 hrs)**

**Note:**
**Total Estimated continuous time from start of 0 (Functional Test)  through end of 17  =  16.0 days (383hrs) - excludes external stim and roll in time (10 hrs)**

**(12 hrs)**

- Power On - Run
- Launch Config

## Thermal Vacuum II (T/V II) Results 

***Thermal Vacuum II (T/V II) Results ***

***Conducted 7/1/00 through 07/17/00***
***All objectives met***
***S-Band Anomaly ***
***Significant characterization performed prior to removal from Chamber***
***Presented later as a Special Topic***
***Additional demonstration of nominal operation of EO-1 spacecraft and payloads at temperature extremes***
***Additional bake-out of ALI and Hyperion instruments***
***Conclusion***
***After S-Band is replaced, EO-1 S/C qualified for on-orbit operation***
***Post Thermal Vacuum Functional Test was nearly flawless***

## Spacecraft CPT Testing

***Spacecraft CPT Testing***

***The CPT contains about 100 individual tests***
***All nominal and critical commands (about 500) tested during CPT***

***Sections 0 and 1: ******	******Power-on defaults, launch, ascent, ******	******deployment, and sun acquisition***
***Sections 2, 5, & 6: ******	******Exhaustive S/C tests: ACS, Power, ******	******C&DH, RF, S/A drive, deployment ******	******redundancy***
***Section 3: ******	******Non-imaging tests with instruments ******	******and WARP***
***Section 4: ******	******EFF***
***Sections 7 & 8: ******	******Exhaustive imaging***
***Sections 9 & 10: ******	******Restart, safemode, & load-shedding***
***Section 11: ******	******Orbit-timeline***

***Post S-Band integration CPT at Launch Site***
***Nearly flawless with a total of 4 minor Problem Reports which have been dispositioned and closed***

**** CPT and additional tests***

## Total Operating Time

## FSW Operating Time

## Projected Total Hours for S-Band Transponder

## I&T Schedule as of 10/5/00

***I&T Schedule as of 10/5/00***

## Action Item Status

*** ******. . . Dale Schulz***
*EO-1 Project Manager*

## Project Databases

***Project Databases***

***Developmental activities were tracked through “community-based” databases***
***There are eight such databases:***
***Project-Level Reviews: ******	****Includes all project-level reviews and all **	**special external, independent reviews such **	**as the Littles Review, Senior Manager’s **	**Review, EIRR, Red Team, and FSW **	**Independent Review.  *
***Spacecraft: ******	****All Problem Reports are included here, **	**including all those from I&T*
***Flight Software: ******	****Contains all FSW changes*
***Operations: ******	****Supports the development of the Ground **	**System as well as all operations  *
***GSFC / NCR: ******	****Supports in-house developments such as the **	**WARP and AC*
***Materials / Processes: ******	****Contains waivers for materials and processes*
***Waivers:******	****Contains waivers to baselined requirements*
***Schedule Liens: ******	****Contains I&T activities not yet incorporated **	**into the baselined schedule*
***Vast majority (>90%) of all entries are in the first four databases***

## Action Item Convergence Prior to Launch

***Action Item Convergence Prior to Launch***

***Currently there are 8 Project Databases***
***By the time the Spacecraft is turned over to Boeing for DPAF integration there will be two -- Project and Operations***
***All pre-launch action items will be closed prior to launch***
***Only a few post-launch action items will transfer to Operations***

## EO-1 Action Item Status

## EO-1 Toteboard of RFAs

## S/C Problem Report (PR) Closure Status

## Launch Campaign Status

*** ******. . . Dale Schulz***
*EO-1 Project Manager*

## EO-1 Spacecraft at VAFB in Clean Room

## Launch Campaign Flow

***Launch Campaign Flow***

- * in parallel with SAC-C processing

## Flight Battery Integration

***Flight Battery Integration***

## S-Band Integration

***S-Band Integration***

## EO-1 in CPT Configuration (9/22/00)With Alignment Equipment Setup

***EO-1 in CPT Configuration (9/22/00)******With Alignment Equipment Setup***

## Fueling Status

***Fueling Status***

***Self-contained Atmospheric Protective Ensemble (SCAPE) Training completed for Primex & Swales Fueling Teams (July 2000)***
***Fueling Drum (4BW) completed re-certification on 9/21/00***
***Hydrazine loaded to 4BW 9/29/00***
***4BW will arrive at VAFB no later than October 9, 2000***
***Primex crew arrives at VAFB October 16, 2000***
***Fueling EO-1 / SAC-C October 17-20, 2000***
***Rev C of Primex Fueling Procedure completed 9/30/00***
***Incorporates specifics associated with Astrotech Facility***
***Spacecraft Configuration and GSE Layout in Astrotech facility finalized***
***TIM held with Swales, Primex and SAC-C 9/15/00***

## EO-1/SAC-C Fueling Setup in the Astrotech West Bay

***EO-1/SAC-C Fueling Setup in the Astrotech West Bay***

**Primex****Fueling****Chief**

- SAC-CControlRoom

## Lab-1 Building 836        (Rooms 10 and 11)

***Lab-1 Building 836******        ******(******Rooms 10 and 11)***

## EO-1 / SAC-C SLC-2 EEB Layout

***EO-1 / SAC-C SLC-2 EEB Layout***