Stennis Space Center Engineering and Test … Powell Engineering and Test Directorate Stennis Space...

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Christine Powell Engineering and Test Directorate Stennis Space Center Engineering and Test Directorate Overview https://ntrs.nasa.gov/search.jsp?R=20120001858 2018-06-23T14:57:29+00:00Z

Transcript of Stennis Space Center Engineering and Test … Powell Engineering and Test Directorate Stennis Space...

Christine Powell

Engineering and Test Directorate

Stennis Space Center Engineering and Test Directorate

Overview

https://ntrs.nasa.gov/search.jsp?R=20120001858 2018-06-23T14:57:29+00:00Z

History of Stennis Space Center

• Construction date—May 1963 • Mississippi Test Facility established—April 23, 1966 • Hancock County, Miss. provided access to

– Isolated test site – Water and road access – Public utility – Supportive community – Climate conducive for year-round testing

• First and second Saturn V stages were tested from 1967-1972 • Renamed John C. Stennis Space Center in 1988 • Nation’s largest rocket engine testing facility

John C. Stennis Space Center was established to test the engines used to propel the Apollo space craft to the moon.

“I don’t know yet what method we will use to get to

the moon, but I do know that we have

to go through Mississippi to get

there!” -Dr. Wernher Von

Braun

13,800 Acre Fee Area 125,000 Acre Buffer Zone

Location

A Unique Federal City

• NASA – John C. Stennis Space Center*

• 280 NASA Civil Servants • 1,420 NASA Contractors

– NASA Shared Services Center* • The NSSC is collocated on site with 440 employees • 120 NASA Civil Servants • 320 NSSC Contractors

• NAVY – Commander, Naval Meteorology & Oceanography Command – Naval Oceanographic Office – Naval Research Laboratory – Naval Small Craft Instruction and Technical School – Navy Special Boat Team 22 – Navy Human Resources Service Center Southeast

• More than 30 major federal, state, academic and private organizations – More than 60 technology-based companies

*employee numbers are approximate

More than 5,000 NASA, Contractor and Resident Agency Employees

Resident Agencies at Stennis Space Center

Department of Interior • USGS Water Resources

Division • USGS Geomagnetism Center

State of Louisiana • Louisiana Technology

Transfer Office

Institute for Technology Development • Spectral Visions

Mississippi Enterprise for Technology • Stennis Technology Enterprise Center

General Services Administration

Department of Defense • Commander, Naval

Meteorology & Oceanography Command

• Naval Oceanographic Office • Naval Research Laboratory • Naval Small Craft Instruction

and Technical Training School • Navy Special Boat Team 22 • Navy Human Resources

Service Center Southeast • Mississippi Army Ammunition

Plant • Defense Contract Management

Command

Department of Commerce • NOAA, NWS, National Data

Buoy Center • NOAA National Marine

Fisheries Service • NOAA National Coastal Data

Development Center

Department of Transportation

• U.S. Coast Guard

Environmental Protection Agency • Environmental Chemistry

Laboratory • Gulf of Mexico Program

Commercial Companies • Pratt and Whitney Rocketdyne • Lockheed Martin, Mississippi

Space and Technology Center • Rolls Royce North America

Major Contractors • Pratt and Whitney Rocketdyne • Jacobs Technology Inc. • Computer Sciences Corp. • Applied Geo Technologies • Paragon Systems Inc. • Science Applications

International Corporation

Center for Higher Learning • Mississippi State University • University of Southern

Mississippi (USM) • USM Center for Marine

Science • University of New Orleans • Pearl River Community

College

University of Southern Mississippi - College of Marine Sciences • Dept. of Marine Science • Center for Ocean and Atmospheric Modeling

State of Mississippi • Mississippi Space

Commerce Initiative Geo Resources

Institute Department of

Energy • Strategic Petroleum

Reserve

SSC Test Area

Apollo

Rocket Propulsion Test Heritage Space Shuttle •First Saturn V

Rocket Engine Test Firing April 23, 1966 •First Space Shuttle Main Engine Test Firing May 19, 1975

•First J-2X Engine Component Test December 18, 2007 •First J-2X Engine Test Firing July 14, 2011

Space Launch System

RS-68 Engine Space Shuttle Main Engine

Orbital/ Aerojet AJ-26

Current/Recent Rocket Propulsion Testing Engines and Components

J-2X Engine

Technical Services For Testing • Systems Engineering

– Requirements, Processes, Priorities, Integration, Life Cycle Reviews, …

• Design and Analysis

• Test Operations

• Support Infrastructure and Labs

E1 DR

E1 ELECTRICAL TPS

E1 MECHANICAL TPS

E2 DR

E2 ELECTRICAL TPS

E2 MECHANICAL TPS

E3 DR

E3 ELECTRICAL TPS

E3 MECHANICAL TPS

Quit Application

E1 E2 E3

E1 Log Book E2 Log Book E3 Log Book

PTD SOIs

E-Complex Work Control

Component Databases

Work ControlGeneral

Guidelines

Guidelines

TPS GeneralGuidelines

Safety/QualityGuidelines

DR GeneralGuidelines

Scheduler’sSmart Menus

System Engineering Test Request Logbook

E1 PreTest Briefing E2 PreTest Briefing E3 PreTest Briefing

Material TransferRequest

DDMS Test DataPTD HOME

TPS Archives

Path to MBSE

• Transition – Moving from a traditional document centric

engineering management system to a model centric architecture

• Intent is to improve data configuration control, data accessibility and reduce costs

• Effort is evolutionary – 10 years into transition – Design and Data Management System (DDMS)

• Primary system tool is Windchill • Also includes a server system (for test data, video, large files)

and a supercomputing cluster (HPCC – for running models and simulations)

SSC PDLM Environment Windchill Based

SSC PDLM Environment • Center Level Implementation to manage project and facility

designs and engineering data, allowing for integration capabilities with customers and partners

• Propulsion/Engine Testing is SSC’s primary responsibility that requires high level of confidence in configuration of test facilities and control/data systems

• Drawing Centric – SSC has historically used primarily AutoCAD, but has started its evolution into Model Based System Engineering with extensive use of Pro-E and other support elements

• Manage design and data for SSC Projects (Commercial, DOD, NASA, Internal) based upon NPR7123.1 System Engineer processes

NASA System Engineering Engine

ReqLink

AutoCad

Pro-E

Key Decision Records

Verification Items

Problem Reports

Validation Items

Work Authorization Documents

Engineering Change Objects

IRMA

Technical Review

Packages

Lessons Learned

Stennis Dissenting

Opinion

Document Types Engineering

Analysis

Stennis Space Center Design and DataManagement System

PortalPage

PDMLink

ProjectLink

RequirementsLink

Stennis Engineering

Objects

ChangeRequest

Stennis LessonsLearned

RequirementsChange Request

EngineeringAnalysis

EngineeringChange Request

EngineeringOrder

DissentingOpinion

TeamCollaboration

ChangeIssue

ProblemReport

Key DecisionRecord

WindchillDocuments

TestRequest

Work AuthorizationDocument

Group BasedLinks

AccessRequest

PasswordChange

Group BasedCalendar

FrequentlyAsked Questions

User Guidesand Videos

CAD DrawingManagement

DocumentManagement

Raw DataManagement

Customer Spec.Management

SpecificationManagement

RequirementsManagement

Upstrem &Downstream Traceability

ChangeAction

WorkSteps

ChangeOrder

Test PreparationSheet

Disposition

DDMSModules

DDMSReports

DDMSLibraries

TPSReports

PRReports

GeneralReports

DrawingReports

Change ObjectReports

AnalysisReports

CommonParts

SSCDocuments

DDMS/Windchill Software Architecture

Stennis Space Center

Requirements Development and Management within DDMS/WindChill RequirementsLink

System Modeling in Pro-E <in work>

Execution of Verification/Validation Assignment and Tracking for Bi-Directional Traceability

Change Management throughout the Project Life via Engineering Change Objects

System Designs

625 ft3 15,000 psig

UHP GH2 Bottles

MV10A89

GH

FCV10A27

GH

FCV10A26

GH

To HPFlare

MV10F22

GH

Mixer

ToCell 3

MV10F21

LH

MV10F20

LH

GF10A4255

LH

VPV10F23

LH

MV10A4269

LH

LPTP

FMVTo HPFlare

TC100GH

PE10A1402

LH

625 ft3 15,000 psig

625 ft3 15,000 psig

PE436GH20 mph Wind

Distance from Discharge (ft)

System and Test Data Analysis

200 204 208 212 216 220

7000

6000

5000

4000

3000

2000

1000

0

TIME SECONDS

Highly effective integration of design and analysis functions, measured by •Minimal design rework •Reduction in facility activation testing •Improved anomaly resolution timeline

Integrated Data Environment

Wrap-Up

• Successes – Current State

• Consolidation of data tools and sets into a single digital environment

– Includes requirements traceability and workflow automation – Includes migration of problem reports and work authorization

documents from the heritage system

• Challenges – Future State: 100% digital environment

• Work steps performed within tool environment • IT security for off site access for customer representatives • Momentum – maintaining forward progress • Funding, time, and manpower constraints

The Ultimate Goal