Attachment_2_-_Launch_Site_Support_Plan_-_Preliminary_March_2019.pdf

LSP-PLN-333.01-LANDSAT9-LSSP

Preliminary March 2019

Launch Services Program

Landsat 9

Launch Site Support Plan

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APPROVAL PAGE

Scope of Agreement

The National Aeronautics and Space Administration (NASA) Launch Services Program (LSP) Flight Planning Board NASA Launch Services Manifest authorizes the launch of this spacecraft (SC). This Launch Site Support Plan (LSSP) is an agreement between the NASA Launch Site Integration Manager (LSIM), the Observatory Project Representative, and the Launch Service Contractor (LSC) documenting the products and services for launch site processing in NASA provided facilities. By signing this LSSP, the NASA LSIM concurs that plans and requirements have been coordinated with the appropriate launch site personnel and commitments have been received by the appropriate parties to provide the required support and services.

The Observatory Project Representative and the LSC signature on the document indicate awareness of and compliance with applicable policies that govern launch site processing as well as validation of their requirements. Launch site processing at Vandenberg Air Force Base (VAFB) is defined in the LSP-UG-332.01, Guide for NASA Spacecraft Processing at Vandenberg Air Force Base.

Signatures

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Revision and Control

Publication of this LSSP is controlled in the NASA Technical Documentation System. Access to the LSSP is available through the VA LSP portal. Revisions to this LSSP are tracked on the page III revision log. Comments, corrections, or updates should be directed to one of the following:

Mark Mertz Launch Site Integration Manager National Aeronautics and Space Administration

VA-E2-A

Telephone: 805-605-3906 Fax: 805-605-3380 E-Mail address: Mark.A.Mertz@nasa.gov

Timothy M. Trenkle Lead Launch Site Support Engineer

a. i. solutions, Inc.

P.O. Box 640, Lompoc, CA 93438 Telephone: 805-605-5993 Fax: 805-605-3921 E-Mail address: timothy.m.trenkle@nasa.gov

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LIST OF EFFECTIVE PAGES

This is the first publication of this document.

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 155 CONSISTING OF:

Page No.

Cover Page 2 thru 155

March 2019

March 2019

LANDSAT 9 LSSP REVISION LOG

Revision Date Published Pages

Affected Change Description Approval

DRAFT

Preliminary

January 2019 All Distribution of the DRAFT Preliminary LSSP

N/A

Preliminary March 2019 All Preliminary Release

March 2019

March 2019

LANDSAT 9 LSSP To-Be-Determined (TBD) / To-Be-Confirmed (TBC) LOG

TBD/

TBC

REQUIREMENT

NUMBER

DESCRIPTION COMMENTS

Table to be used at Baseline Release if required

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March 2019

TABLE OF CONTENTS

LIST OF EFFECTIVE PAGES

LANDSAT 9 LSSP REVISION LOG

LANDSAT 9 LSSP To-Be-Determined (TBD) / To-Be-Confirmed (TBC) LOG

ABBREVIATIONS AND ACRONYMS

SPACECRAFT PROJECT DESCRIPTION

LAUNCH SITE PROCESSING

2.1 LANDSAT 9 SPACECRAFT LAUNCH SITE PROCESSING

2.1.1 Landsat 9 SPACECRAFT LAUNCH SITE ACTIVITIES

2.1.2 SPACECRAFT PROCESSING REQUIREMENTS AND SPECIAL

AGREEMENTS

2.2 ATLAS V PROCESSING REQUIRING NASA LSP SUPPORT

2.2.1 ATLAS V PROCESSING ACTIVITIES IN NASA LSP FACILITIES

2.3 LAUNCH SITE CONTINGENCY PLANNING

2.3.1 Severe Weather/Natural Disasters

2.3.2 Wild Fires/Controlled Burns

2.3.3 Emergency Plan for Processing Facility

2.3.4 Power Outages

2.3.5 Launch Scrub/Turnaround

2.3.6 Emergency Fuel Off-Load

2.3.7 Lightning Response

REFERENCE EXHIBITS

SPACECRAFT SUPPORT REQUIREMENTS AND COMM MATRIX

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ABBREVIATIONS AND ACRONYMS

The following abbreviations and acronyms are used in this document.

Ø Phase

30SW 30th Space Wing

A Ampere ACS American Chemical Society Admin Administrative ADMS Automated Data Management System AF Air Force AFSPCMAN Air Force Space Command Manual Ahr Amp-hour AHU Air Handling Unit AKA Also Known As AL Airlock AM Amplitude Modulated ANSI American National Standards Institute ASTM American Society for Testing and Materials ATLO Assembly, Test, and Launch Operations

B Building BCE Bench Checkout Equipment BLDG Building BRB Battery Relay Box

C Celsius CAT Category CC Communication Coordination CCAFS Cape Canaveral Air Force Station CCI Controlled Cryptographic Items CCP Contamination Control Plan CCTV Closed-Circuit Television CD Compact Disc CDR Critical Design Review CDRL Contract Data Requirements List CEMP Consolidated Comprehensive Emergency Management Plan CFM or cfm Cubic Feet per Minute CGA Compressed Gas Association CLC Closed Loop Certification CLM Cubic Liters per Minute CLN RM Cleanroom CNT RM Control Room COMM Communication COMSEC Communications Security COORD Coordination CPT Comprehensive Performance Test

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ABBREVIATIONS AND ACRONYMS – (Cont’d)

CR Cleanroom CSU/DSU Channel Service Unit/Data Service Unit CWA Clean Work Area

DECON Decontamination DHCP Dynamic Host Configuration Protocol DI Deionized (Water) DOT Department of Transportation DSN Deep Space Network DVD Digital Video Disc

ECS Environmental Control System EGSE Electrical Ground Support Equipment EI End Instrument ELSA Emergency Life Support Apparatus ELV Expendable Launch Vehicle EMI Electromagnetic Interference ENG or Eng. Engineer/Engineering Environ Environment EPO Emergency Power Off EQUIP Equipment ER Eastern Range ESD Electrostatic Discharge EWR Eastern/Western Range

F Fahrenheit FAX Facsimile FN Foreign National FOD Foreign Object Debris FONSI Finding of No Significant Impact FPLA Flight Payload Adapter FPM or fpm Feet per Minute FR Fire Retardant FSO Facility Security Officer FT or ft Foot FTS Federal Telecommunications System

GFE Government Furnished Equipment GHe Gaseous Helium GHz Giga-Hertz (Hertz x 10E9) GLVI GSFC Launch Vehicle Integration GMT Greenwich Mean Time (UTC, Zulu) GN2 Gaseous Nitrogen GOP Ground Operations Plan GOR Ground Operations Review GOWG Ground Operations Working Group

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ABBREVIATIONS AND ACRONYMS – (Cont’d) GPS Global Positioning System GPTU Generic Propellant Transfer Unit GSE Ground Support Equipment GSFC Goddard Space Flight Center

H Height HD High Definition HEPA High Efficiency Particle Arrestor HPF Hazardous Processing Facility HPM Hydrazine Propulsion Module HSF Hazardous Storage Facility HVAC Heating, Ventilation, Air Conditioning Hz Hertz

I&T Integration and Test IAW In Accordance With ICD Interface Control Document IEST Institute of Environmental Sciences and Technology I/F Interface IFD In-Flight Disconnect ILC Initial Launch Capability IP Internet Protocol IPA Isopropyl Alcohol (same as 2-Propanol) ipm Inches per Minute IRIG Inter-range Instrumentation Group ISO International Organization for Standardization ISP Internet Service Provider

KHz Kilo Hertz KSC John F. Kennedy Space Center KTI Kennedy Technical Instruction kVA Kilovolt-Ampere

L Length LAN Local Area Network lbf Pounds-force

lb. Pound lbs. Pounds LCD Liquid Crystal Display LDCM Landsat Data Continuity Mission LN2 Liquid Nitrogen LOC Location LPD Launch Preparation Document (ULA) LPM Litres per minute LRR Launch Readiness Review LSC Launch Service Contractor LSOTP Launch Site Operations and Test Plan

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ABBREVIATIONS AND ACRONYMS – (Cont’d) LSIM Launch Site Integration Manager LSP Launch Services Program LSSE Launch Site Support Engineer LSSP Launch Site Support Plan LV Launch Vehicle LVIS Launch Vehicle Interface Simulator LVRT Launch Vehicle Readiness Test

Max Maximum MBPS Megabits per Second MCE Mission Comm Engineer MDC Mission Director’s Center MFP Multi-Function Printer MGSE Mechanical Ground Support Equipment MHz Mega-Hertz (Hertz x 10E6) MIL-PRF Military Performance Specification MIL-STD Military Standard Min Minimum or Minute MISC Miscellaneous MM Mission Manager MOC Mission Operations Center MOE Mission Operations Element MOU Memorandum of Understanding MPCP Mishap Preparedness and Contingency Plan MSDS Material Safety Data Sheet MSPSP Missile System Prelaunch Safety Package MSSCS Modular Spacecraft Shipping Container System MST Mobile Service Tower

N Newton N/A or NA Not Applicable NASA National Aeronautics and Space Administration NEMA National Electrical Manufacturers Association NEPA National Environmental Policy Act NET No Earlier Than NGIS Northrop Grumman Innovation Systems NISN NASA Integrated Services Network NLS NASA Launch Services (Contract) NLT No Later Than NPR NASA Procedural Requirement NSA National Security Agency NSC NASA Spacecraft Coordinator NSI NASA Standard Initiator NTE Not to Exceed NTR Network Timing Reference NTSC National Television System Committee (a standard) NVR Non Volatile Residue

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ABBREVIATIONS AND ACRONYMS – (Cont’d) OD Operation Directive Document (Range Document) OJT On-the-Job Training OLI-2 Operational Land Imager 2 OLM Observatory Launch Operations Manager OPS or Ops Operations OR Operational Requirements Document (Range Document) ORT Operational Readiness Test OSHA Operational Safety and Health Administration

PAO Public Affairs Office (Outreach) PCA Payload Controlled Area PCM Pulse Code Modulation PDR Preliminary Design Review PDU Power Distribution Unit P/L Payload PLA Payload Adapter PLF Payload Fairing PMEL Precision Measurement Equipment Laboratory PMF Payload Mate Fixture POC Point of Contact POTS Plain Old Telephone System PPB or ppb Part per Billion PPF Payload Processing Facility PPM or ppm Part per Million PRP Personnel Reliability Program PSI Payload Safety Introduction PSIA Pounds Per Square Inch - Absolute PSIB Payload Safety Introduction Briefing PSIG Pounds Per Square Inch - Gauge PSWG Payload Safety Working Group

RBF Remove Before Flight REQ Requirement REV Revision RF Radio Frequency RH Relative Humidity RSDO Rapid Spacecraft Development Office RTA Radial Telescope Assembly

S/A Solar Array SAS Solar Array Simulator SBCEPA Santa Barbara County Environmental Protection Agency S/C or SC Spacecraft SCAPE Self Contained Atmospheric Protective Ensemble SCFH Standard Cubic Feet Per Hour SCFM Standard Cubic Feet Per Minute

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ABBREVIATIONS AND ACRONYMS – (Cont’d) SCIT Spacecraft Integration and Test rack SCOUT Spacecraft Operations Utility Trailer SDP Safety Data Package SDS Safety Data Sheet SIS Spacecraft Interface Simulator SLC-3E Space Launch Complex-3 East SMD Science Mission Directorate SOW Statement-of-Work

sq. Square SS Stainless Steel SSPP Systems Safety Program Plan STD Standard STF Structural Transport Frame STM Safe to Mate STV Spacecraft Transport Vehicle SV Space Vehicle SVTL Safety Verification Tracking Log SW Space Wing

TAA Technical Assistance Agreement TBC To-Be-Confirmed TBD To-Be-Determined TBR To-Be-Reviewed TBS To-Be-Supplied TC Test Conductor TIRS-2 Thermal Infrared Sensor-2 TM Telemetry TVAC Thermal Vacuum

UDS Universal Documentation System UHF Ultra High Frequency ULA United Launch Alliance UPC United Paradyne Corporation UPS Uninterruptable Power Supply USGS United States Geological Survey UTC Coordinated Universal Time (Zulu or Greenwich Mean Time, GMT) UT Umbilical Tower

VAC Volts AC (Alternating Current) VAFB Vandenberg Air Force Base VDL Voice Direct Line V/M Volt per meter VTS Vandenberg Tracking Station

W Width WAN Wide Area Network WR Western Range WX Weather

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REFERENCE DOCUMENTATION AND PROCESSING GUIDELINES

The following list of references is provided for use in planning and implementing a launch site processing flow in accordance with local, state, and federal regulations.

Launch Site Requirements Documentation

1. KNPR 1860.2 KSC Non-Ionizing Radiation Protection Program

2. KNPR 8715.3 KSC Safety Practices Procedural Requirements

3. NPR 8621.1 NASA Procedural Requirements for Mishap and Close

Call 4,Reporting, Investigating and Recordkeeping

4. KTI-5212 Material Selection List for Plastic Films, Foams and

Adhesive Tapes

5. NPR 8715.7 Expendable Launch Vehicle Payload Safety Program

6. NPR 1600.1 NASA Security Program Procedural Requirements

7. KNPR 1600.1 KSC Security Procedural Requirements

8. KNPD 1800.2 KSC Hazard Communication Program

9. KNPR 8715.2 Consolidated Comprehensive Emergency

Management Plan (CEMP) 10 KNPR 8500.1 KSC Environmental Requirements

11. ISO 14644-1 Cleanrooms and Associated Controlled Environments

– Part 1: Classification of Air Cleanliness by Particle Concentration

12. ISO 14644-2 Cleanrooms and Associated Controlled Environments

– Part 2: Monitoring to Provide Evidence of Cleanroom Performance Related to Air Cleanliness by Particle Concentration

13. ISO 14644-3 Cleanrooms and Associated Controlled Environments

– Part 3: Test Methods

14. IEST-STD-CC1246 Product Cleanliness Levels and Contamination Control Program

15. ASTM-E-1235 Standard Test Method for Gravimetric Determination of Nonvolatile Residue in Environmentally Controlled Areas for Spacecraft

16. ANSI Z136.1 American National Standard for Safe Use of Lasers

17. MIL-PRF-27407C Propellant, Pressurizing Agent, Helium

18. MIL-PRF-27401F Propellant, Pressurizing Agent, Nitrogen

19. CGA G-7.1 Commodity Specification for Air

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Launch Site Reference Documentation

1. PPF (TBS) Facility Safety Manual/Plan

2. PPF (TBS) Payload Processing Facility Handbook/Manual

3. LSP-UG-332.02 Guide for NASA Spacecraft Processing at Vandenberg AFB

4. LSP-UG-411.04 NASA VAFB Facilities Reference Handbook

5. LSP-PR-362.01 Vandenberg Air Force Base (VAFB) NASA Facilities

Operational Safety Plan

6. OD 03200 NASA Generic Test Operations Directive (OD)

Launch Service Contractor and Range Documentation

1. AFSPCMAN 91-710 Range Safety User Requirements Manual

2. NASA-STD-8719.24 NASA Expendable Launch Vehicle Payload Safety

Requirements

3. ULA-ATLAS-ICD-0077 Landsat 9 / Atlas V Interface Control Document

4. L9-08-01 Launch Services Interface Requirements Document

5. L9-08-03 Annex to the Landsat 9 Launch Services Requirements

Document

6.

7.

8.

VAFB-OSP-001

ULA TCD QSMS-

SHEA-001

AWS-FAC-804

ULA Vandenberg Operations Safety Plan Non-ULA Owned Crane Evaluation Data Package

SLC-3E Emergency Guidelines

Landsat 9 Project Documentation

1. 6515-PP65101 Landsat 9 Launch Site Ground Operations Plan

2. 6515-PP64100 Landsat 9 Storage, Transportation and Handling Plan 3.

4.

L9-03-22 L9-03-21

Landsat 9 Transportation Support Plan Landsat 9 Launch Site Contamination Control Plan

5. 6515-DG23800 Landsat 9 Safety Data Package

6. (TBS) Landsat 9 Lightning Strike and Response Plan 7.

8.

(TBS)

(TBS)

Landsat 9 Emergency Off-Load Plan Landsat 9 Contamination Control Plan

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SPACECRAFT PROJECT DESCRIPTION

The following organizations are involved in the concept, design, development, and launch of the Landsat 9 Observatory:

Sponsored by Earth Science Missions Program Managed by Goddard Space Flight Center (GSFC) Manufactured by Northrop Grumman Innovations Systems (NGIS) Processed at (TBD) Payload Processing Facility (PPF), Vandenberg AFB, CA Launched by United Launch Alliance (ULA) on an Atlas V

The Landsat 9 mission will provide continuity in the multi-decadal Landsat land surface observations to study, predict, and understand the consequences of land surface dynamics using repetitive acquisition of high resolution multispectral data of the Earth's surface on a global basis. The data from the Landsat spacecraft series constitute the longest record of the Earth's continental surfaces as seen from space. It is a record unmatched in quality, detail, coverage, and value.

1.1 Landsat 9 Mission Objectives

The major mission objectives are summarized as follows:

a. Collect and archive reflective multispectral image data affording seasonal coverage of the global land mass for a period of no less than five years with the Operational Land Imager 2 (OLI-2) instrument. Collect and archive thermal multispectral image data affording seasonal coverage of the global land mass for at least three years with the Thermal Infrared Sensor-2 (TIRS-2) instrument.

b. Ensure that Landsat 9 data are sufficiently consistent with data from the earlier Landsat missions, in terms of acquisition geometry, calibration, coverage characteristics, spectral characteristics, output product quality, and data availability to permit studies of land cover and land use change over multi-decadal periods.

c. Distribute Landsat 9 data products to the general public on a nondiscriminatory basis.

GSFC has the responsibility for overall project management. The Landsat 9 Observatory is manifested to launch on a ULA Atlas V 401 vehicle from Space Launch Complex (SLC)- 3E at Vandenberg Air Force Base (VAFB). Landsat 9 is expected to launch in 2020.

Further information on the Landsat 9 project can be found on the World Wide Web at https://landsat.gsfc.nasa.gov/landsat-9/. Information relating to ULA can be found on the World Wide Web at http://www.ulalaunch.com/

1.2 Landsat 9 Observatory

The Landsat 9 Observatory consists of the spacecraft bus provided by NGIS, the Operational Land Imager 2 (OLI-2) developed by Ball Aerospace, and the Thermal Infrared Sensor-2 (TIRS-2) developed by NASA Goddard Space Flight Center. Figure 1.1 shows the launch configuration of the Landsat 9 Observatory.

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Figure 1.1. Landsat 9 Observatory Launch Configuration

The Landsat 9 observatory bus is similar to that of the Landsat Data Continuity Mission (LDCM), which used an existing Rapid Spacecraft Development Office (RSDO) catalog item with mission specific modifications. The observatory bus design solution is mission driven, configuring the bus to accommodate the Instruments and support the science mission. This design achieves all specified science interface goals, balancing Landsat-unique interfaces and the LeoStar-3 architecture. The solar array is a single three panel wing that is mounted and deployed low on the observatory. This arrangement minimizes instrument field of view obstruction. The observatory contains a (TBS) Ahr Lithium-ion battery. The propulsion system is a mono-propellant surface tension single tank design with a diaphragm for propellant management and slosh control using high purity anhydrous hydrazine, eight 22N (5 lbf) thrusters, two service valves, three pressure transducers, two filters, two latch valves, and a cavitating venturi. The observatory bus design includes interlocked primary and redundant operational power feeds to each instrument and survival power feeds that are enabled at all times. The instrument bench is mechanically supported and thermally isolated by three titanium flexures. The metallic (aluminum and titanium) structure is stiffness driven to meet the Atlas V environments. An expanded view of the observatory is provided in Figure 1.2.

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LAUNCH SITE PROCESSING

The Observatory will be integrated and functionally tested by NGIS in Gilbert, Arizona.

Upon completion of Integration and Test, NGIS will deliver the Observatory to the LSP contracted Payload Processing Facility (PPF) at VAFB. NGIS will lead the pre-launch processing activities with support from GSFC, along with associate partners and subcontractors. ULA will perform mechanical and electrical integration with the launch vehicle, and coordinate all operations at SLC-3E. NASA KSC Launch Services Program (LSP) will provide coordination between the Landsat 9 program and ULA and between the program and VAFB/KSC range entities.

The Observatory Project has prime responsibility for Observatory assembly, test, and servicing while processing at the launch site. NASA LSP VAFB provides unique support services to the Landsat 9 Project at the launch site. The NASA Launch Site Integration Manager (LSIM) is responsible for arranging, coordinating, and verifying the agreed to launch site support services for Landsat 9. An overview of the processing and agreements for Landsat 9 is listed in section 2.1.

The Launch Service Contractor (LSC) has prime responsibility for launch vehicle hardware assembly, test, and servicing while processing in NASA LSP provided facilities. NASA LSP provides support services to the LSC at NASA LSP provided facilities for the work necessary for Landsat 9 / Atlas V integration activities. The NASA LSIM is responsible for arranging, coordinating, and verifying these NASA LSP facility support services for the Atlas V. An overview of the processing and agreements for Atlas V is listed in section 2.2.

Section 2.3 describes special contingency situations, agreements, and support services that may be required by Landsat 9 while at the launch site.

2.1 LANDSAT 9 OBSERVATORY LAUNCH SITE PROCESSING

The detailed launch site processing products and services requested by the Observatory Project are listed in the Landsat 9 Support Requirements (Tables 4.1 and 4.2). The LSIM and the Launch Interface Manager have developed the detailed launch site processing requirements for the observatory, and the commitment for providing these requirements as listed. At the Baseline publication of this LSSP, all requirements in Tables 4.1 and 4.2 with a To-Be-Determined (TBD) in the Y/N column will be worked in a timely manner for final resolution prior to their need.

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2.1.1 Landsat 9 Observatory Launch Site Activities

The Observatory will be transported, via ground transportation, from the NGIS Integration and Test Facility in Gilbert Arizona, to the NASA LSP contracted PPF at VAFB, California, where it will undergo final integration, testing, and launch. NASA LSP is providing the contracted commercial PPF (TBD) for the Observatory Project to conduct pre-launch processing.

After Observatory standalone processing is completed, it will be encapsulated in the payload fairing at the PPF and then transported by trailer to the launch site at SLC-3E for final integrated testing, processing, and launch. Major launch site activities are comprised of the following:

a. Arrival, setup and inspection

b. Observatory stand-alone testing

c. Observatory fueling operations

d. Observatory inspections and close-out activities

e. Launch rehearsals

f. Integrated operations with launch service provider

g. Pack-up and departure activities (following launch)

A diagram of the launch site processing flow activities is included as Figure 2.1.

Figure 2.1. Landsat 9 Launch Site Processing Flow

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2.1.2 Observatory Processing Requirements and Special Agreements

The following are Observatory-unique processing requirements and special agreements between the Observatory Project and launch site personnel:

a. Cleanliness requirements:

Landsat 9 components have contamination sensitive surfaces that will require ISO 7 clean work areas. The Landsat 9 instruments are susceptible to contamination from molecular contaminants, moisture and particulates. Guidelines for continuous contamination control, monitoring, sampling, and cleaning of the applicable facilities are included in the Landsat 9 Launch Site Contamination Control Plan (L9-03-21).

b. Purge requirements:

A continuous Gaseous Nitrogen (GN2), Grade C purge will be required for both the OLI-2 and TIRS-2 instruments.

Flow Rate and Pressure: as specified in Table 4.1 Outages allowed are: no more than a 30 minute outage per occurrence with a maximum interruption of no more than 30 minutes in a 24 hour period.

GN2 will be required for transport operations and integrated operations with the launch service provider through launch.

The Battery Relay Box (BRB) uses GN2 for purge while connected to the Observatory at the PPF after fueling. Grade B GN2 is acceptable in the PPF and shop grade (or better) for purge while connected to the Observatory (outside of the clean tent) at SLC- 3E is acceptable.

c. Special transportation requirements:

An instrument Grade C GN2 purge will be maintained during fairing installation, pre-transport staging, and during transport to SLC-3E.

During transport to SLC-3E, RF levels to be restricted to 10V/m at all frequencies controllable by the Western Range.

d. Special handling guidelines:

The RF environment shall be restricted to 10V/m at the Payload Processing Facility and at the SLC-3E launch site at all frequencies controllable by the Western Range.

e. Landsat 9 Project specific training required for access to observatory processing areas:

COMSEC training ESD training Landsat 9 clean work area practice training

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f. Use of special Work Time Policy:

The Landsat 9 Observatory launch team (GSFC and NGIS personnel) will comply with NASA Work Time Policy KNPR 8715.3 and Air Force Work Time policy requirements of NASA-STD-8719.24.

g. Tool Control Plan:

Observatory launch team to provide a tool control plan in accordance with KNPR 8715.3, section 5.1.

h. Communications Security (COMSEC):

1) COMSEC materials are installed on the Observatory and the Radio Frequency (RF) rack. COMSEC keying materials, in a COMSEC safe, will accompany the RF Rack electrical GSE (EGSE) at all times. The Observatory, RF Rack and COMSEC safe will have access limitations at all times.

2) Only designated personnel with COMSEC training may have unescorted access to the area where the Observatory is located in the PPF prior to encapsulation or anytime the mission unique fairing door is off after encapsulation.

3) Personnel with COMSEC training may have unescorted access to the area where the Observatory is located in the PPF or pad after encapsulation as long as the mission unique fairing door is installed.

4) Only designated personnel with COMSEC training may have unescorted access to the area where the RF rack is located in the PPF.

5) Un- briefed personnel must be escorted by a cleared person at all time when in those areas with the Observatory or RF rack.

j. Special contamination restrictions:

The PPF operator will ensure that there are no silicone-based materials used in the clean work areas. Restricted materials include adhesives, adhesive tapes, films, lubricants, and cleaning materials. In addition, storage of any silicone-based materials in the clean work areas is to be prohibited.

2.2 ATLAS V PROCESSING REQUIRING NASA LSP SUPPORT

Detailed launch site processing requirements requested by the LSC while processing in a NASA LSP provided facility are negotiated by the LSIM and the LSC Representative.

Launch site processing products and services requested by the launch vehicle contractor are included in the attached Support Requirements (Tables 4.1 and 4.2). Any requirements in Tables 4.1 and 4.2 with a TBD listed in the Y/N column will be resolved in a timely manner prior to need.

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2.2.1 ATLAS V Processing Activities in NASA LSP Facilities

The following LSC standalone and integrated activities in the NASA LSP provided facilities require NASA-coordinated launch site support. These activities require coordination between the LSIM, Landsat 9 Project, and the LSC.

a. Equipment space and operations at PPF

b. Office space at the PPF

c. Payload Fairing and GSE preparations

d. Continuous Observatory GN2 purge through PLF installation closeouts

e. Observatory mate to the launch vehicle adapter

f. Separation system installation

g. Observatory encapsulation

h. Observatory transportation to SLC-3E and mate to the launch vehicle

Detailed launch site processing requirements requested by ULA for the payload launch site flow are negotiated by the LSIM and ULA Mission Integration. Launch site-processing products and services requested by the launch vehicle provider are included in Table 4.1.

Ground Support Equipment (GSE) the LSC plans to locate in the PPF is listed in Table 3.3.

2.2.2 LSC Processing Requirements and Special Agreements

The following are LSC unique processing requirements and special agreements between the LSC and the LSIM for the activities in the NASA-Provided PPF:

a. PPF Assigned Space:

The PPF area provided for the fairing alignment activities must be the same area that will be used for Observatory encapsulation. Once the fairing processing has started, it cannot be exposed to less than an ISO class 8 cleanroom environment.

2.3 LAUNCH SITE CONTINGENCY PLANNING

Special consideration should be given to contingency situations such as emergency off-load of propellants, scrub turnaround, and launch termination. The customer must develop a written plan and procedures for input to contingency operations as listed here. For launch delays that require removal of the Observatory from the launch vehicle, the sequence of flow is typically the reverse of the installation sequence.

2.3.1 Severe Weather/Natural Disasters

Vandenberg AFB is in an area that may be subject to seismic activity. Observatory, GSE, handling fixtures or other support equipment will be evaluated to determine need for seismic restraint.

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2.3.2 Wild Fires/Controlled Burns

Occasional wildfires may overtax the filters in a cleanroom facility. If extremely contamination sensitive, a plan for bagging or protecting the observatory should be developed for this possibility. Additionally, outside air dampers serving the AHU’s that supply the clean air to the payload areas shall be closed.

Facilities Burn Control Restriction: Control burns within a one mile radius or in direct path (wind vector) of fuel source are prohibited.

2.3.3 Emergency Plan for Processing Facility

Emergency egress and rendezvous plans will be made available for all facilities occupied by Landsat 9 launch team personnel. Emergency call lists will be developed upon Observatory arrival at the launch site.

2.3.4 Power Outages

Uninterrupted power systems are available at the PPF and Bldg 836 for EGSE and critical facility circuits. Standby generators are present at these locations and should come online before UPS depletion. However, if the Observatory would be adversely impacted by the failure of a standby power generator to start before UPS depletion, the project should develop contingency plans for a controlled Observatory shutdown.

The PPF shall provide a Facility Power Outage & Recovery Checklist to identify impact of a power loss to the facility to spacecraft dedicated circuits, work area lighting, facility monitoring and safing sytems, security systems, cranes, doors, and any other dependent facility supplied items to provide insight and awareness for the Project to prepare for ensuring safe securing of operations. Included shall be the necessary recovery steps and timelines to enable a safe and expedient return to processing.

NOTE: SLC-3 does not have standby generators for backup power.

2.3.5 Launch Scrub/Turnaround

The project should develop a plan for any observatory battery charging, maintenance or replacement of items that may occur during a prolonged launch delay.

2.3.6 Emergency Fuel Off-Load

ULA procedure AWS-FAC-804, SLC-3E Emergency Guidelines, provides the procedures, checklists, and contacts for emergencies at SLC-3E. The Project will provide the Landsat 9 Emergency Offload Plan (a situation-specific procedure will be developed as necessary at the time of an anomaly).

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2.3.7 Lightning Response

The Landsat 9 project team will respond to Lightning Watch and Warnings as prescribed in NASA-STD-8719.24.

The Observatory Project has developed a Lightning Response Plan and Observatory state-of-health retest sequence to be used at either the PPF or the launch pad if an area near-strike has occurred or is suspected to have occurred (Pad Aliveness Test or Comprehensive Performance Test depending on the severity of the as-measured or suspected near-strike; note that a Comprehensive Performance Test can only be performed while at the PPF and not encapsulated by the payload fairing. Should a Comprehensive Performance Test be required due to a near strike after arrival at SLC-3E it would require de-stack of the spacecraft and return to the PPF for de-encapsulation).

REFERENCE EXHIBITS

Submittal of required documents or items specified for use at the launch site by the Observatory provider and the launch vehicle provider that require review and/or approval are classified as Launch Site Deliverables and are coordinated with the LSIM. Table 3.1 provides the listing of the Launch Site Deliverables with respective planned submittal dates offset from the Initial Launch Capability (ILC) date and their status. Following publication of this LSSP Baseline, Table 3.1 will be updated subsequently as needed outside of a new release to the LSSP. Contact the LSIM to obtain the latest copy of the Launch Site Deliverables list.

Ground Support Equipment (GSE) the Observatory plans to bring to the launch site is listed in Table 3.2. GSE the LSC plans to locate in the PPF is listed in Table 3.3.

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Table 3.1 Launch Site Deliverables

VAFB Arrival: 9 Oct 2020 Launch: 15 Dec 2020 Revised: 25 Mar 2019

Item # Item Source

Requirement for Item

Launch Site Response to Item

Submittal Requirements and

Delivery Requirements

Need Date Landsat 9 Submittal

Date

LV

Submitta l Date Status

LS1 Launch Site Requirements Development

LS1.1 Provide Program Introduction or Mission Concept Briefing. This can be held in conjunction with the Payload Safety Introduction

(PSI)

UDS Users Guide

AFSPCM 91-710

Briefing 36-48 months prior to launch

31.Dec.2017 09.May.2017 N/A Closed

LS1.2 Provide the appropriate representation and participation at GOWG’s

- Provide presentations required by the co-developed agenda

BOSS

LSP-UG-332.01

LSP-UG-332.02

Minutes 1 week prior to

GOWG

Typically 2 times a year depending on mission life cycle stage and mission complexity

05.Dec.2018 05.Dec.2018 05.Dec

Closed

LS1.3 Provide requirements to LSIM for Preliminary Launch Site Support Plan (LSSP)

a. Provide a preliminary ground operations flow plan (launch site operations plan)

b. Provide preliminary launch site computer networking requirements

LSP-UG-332.01

LSP-UG-332.02

Draft LSSP 17-27 months prior to SC arrival

28.Feb.2019 18.Mar.2019 25.Mar

Closed

LS1.4 Submit Non-Standard Security Requirements (COMSEC, RTGs, etc.)

NPR 1600.1 Draft LSSP 17-27 months prior to SC arrival

18.May.2019 18.Mar.2019 N/A Closed

LS1.5 Submit Non-Standard Contamination Requirements or Contamination Control Plan

Payload Specific Draft LSSP Approved CCP

17-27 months prior to SC arrival

18.May.2019 12.Mar.2019 N/A Closed

LS1.6 Provide concurrence for Preliminary LSSP Release

LSP-UG-332.01

LSP-UG-332.02

Released Preliminary

LSSP

11-24 months prior to SC arrival

01.Apr.2019 25.Mar.2019 25.Mar

March 2019

Table 3.1 Launch Site Deliverables (Cont’d)

VAFB Arrival: 9 Oct 2020 Launch: 15 Dec 2020 Revised: 25 Mar 2019

Item # Item Source

Requirement for Item

Launch Site Response to Item

Submittal Requirements and

Delivery Requirements

Need Date Landsat 9 Submittal

Date

LV

Submitta l Date Status

LS1.7 Provide inputs for Baseline

LSSP

LSP-UG-332.01

LSP-UG-332.02

Final Draft LSSP 5-7 months prior to SC arrival

12.May.2020

LS1.8 Provide final inputs/signature for Baseline LSSP release

LSP-UG-332.01

LSP-UG-332.02

Released Baseline

LSSP

4 months prior to hardware arrival at

PPF

11.Jun.2020

LS1.9 Provide the appropriate representation and participation at the GOR

a. Provide a presentation on spacecraft status and readiness to ship to the launch site

BOSS

LSP-UG-332.01

LSP-UG-332.02

Minutes Launch Site Readiness to Receive S/C

GOR held ~ 1 month prior to arrival

Submit charts 1 week prior to GOR

09.Sep.2020

LS2 Launch Site Operations

LS2.1 Submit Environmental Impact Analysis (AF Form 813)

NEPA FONSI or Handling Requirements

9 months prior to SC arrival

13.Jan.2020 N/A

LS2.2 Materials Control

LS2.2.1 Submit list (& test samples as required) of GSE plastics, films, & adhesives used

KTI-5212 Rev. D maptis.nasa.gov

Testing results for samples

List approval for use in facilities

5-9 months prior to SC arrival

12.May.2020 N/A

LS2.2.2 Submit Safety Data Sheets

(MSDS)

KNPR 1840.1 Availability for all personnel working near spacecraft

30 - 60 days prior to arrival

10.Aug.2020 N/A

LS2.3 Hazardous Waste Management

LS2.3.1 Provide the point of contact for waste management

LSP-UG-332.01

LSP-UG-332.02

KNPR 8500.1

Compliance with Environmental

Regulations

6 months prior to arrival

09.Sep.2020

March 2019

Table 3.1 Launch Site Deliverables (Cont’d)

VAFB Arrival: 9 Oct 2020 Launch: 15 Dec 2020 Revised: 25 Mar 2019

Item # Item Source

Requirement for Item

Launch Site Response to Item

Submittal Requirements and

Delivery Requirements

Need Date Landsat 9 Submittal

Date

LV

Submitta l Date Status

LS2.3.2 Provide hazardous waste management information

For KSC and VAFB processing

a. Submit KSC Form 26-551 "Process Waste Questionnaire"

b. Submit Waste Management Training memo

For Commercial processing

a. Submit chemicals list for commodities (if list is not included in the MSPSP)

b. Coordinate with the LSIM and PPF Mission Manager if hazardous waste will be generated. PPF will assume responsibility for labeling, storing, and disposing of hazardous waste.

LSP-UG-332.01

LSP-UG-332.02

KNPR 8500.1

Compliance with Environmental

Regulations

6 months prior to arrival

12.Apr.2020 N/A

LS2.4 Radiation Control

LS2.4.1 Ionizing Radiation Source Use Authorization

KNPR 1860.1 Approval to process/operate at the appropriate facility.

4 months prior to arrival

11.Jun.2020 N/A

LS2.4.2 Ionizing Radiation User Requirements

KNPR 1860.1 Approval to process/operate at the appropriate facility.

4 months prior to arrival

11.Jun.2020 N/A

LS2.4.3 Ionizing Radiation Transportation to/from NASA Property

KNPR 1860.1 Approval to process/operate at the appropriate facility.

4 months prior to

11.Jun.2020 N/A

March 2019

Table 3.1 Launch Site Deliverables (Cont’d)

VAFB Arrival: 9 Oct 2020 Launch: 15 Dec 2020 Revised: 25 Mar 2019

Item # Item Source

Requirement for Item

Launch Site Response to Item

Submittal Requirements and

Delivery Requirements

Need Date Landsat 9 Submittal

Date

LV

Submitta l Date Status

LS2.4.4 Nonionizing Radiation Source Use Authorization

KNPR 1860.2 Approval to process/operate at the appropriate facility.

4 months prior to arrival

11.Jun.2020 N/A

LS2.4.5 Non-Ionizing Radiation User Requirements

For Commercial Facilities Processing

a. Submit a summary of personnel training and experience

KNPR 1860.2 Approval to process/operate at the appropriate facility.

4 months prior to arrival

11.Jun.2020 N/A

LS2.4.6 Submit information to the LSIM so they can obtain Radio Frequency Authorization/ Coordination Forms

For VAFB launch the LSIM will coordinate with range scheduling for RF frequency authorization

Approval to operate on VAFB/30th Range and

KSC/ 45th Range

4 months prior to arrival

11.Jun.2020 N/A

LS2.5 Launch Site Procedures

LS2.5.1 Submit list of all Customer launch site procedures (Hazardous & Non-Hazardous)

AFSPCM 91-710 90 days prior to arrival

11.Jul.2020

LS2.5.2 Submit Hazardous Procedures AFSPCM 91-710

KNPR 8715.3

Approved Procedure and authorization to use

55 days prior to first use

15.Aug.2020

LS2.5.3 Submit Non-Hazardous Procedures

ASO Safety Manual

Approved Procedure and authorization to use

10 days prior to first use

29.Sep.2020

LS2.5.4 Submit final transportation plan/schedule and arrival day badging request

LSP-UG-332.01

LSP-UG-332.02

Approved Plan and Badging

30 -45 days prior to

09.Sep.2020 N/A

March 2019

Table 3.1 Launch Site Deliverables (Cont’d)

VAFB Arrival: 9 Oct 2020 Launch: 15 Dec 2020 Revised: 25 Mar 2019

Item # Item Source

Requirement for Item

Launch Site Response to Item

Submittal Requirements and

Delivery Requirements

Need Date Landsat 9 Submittal

Date

LV

Submitta l Date Status

LS2.5.5 Submit Hurricane Plan KDP-KSC-P-

LSP-TI-362.01

Approved Plan and authorization to be on KSC, ASO or CCAFS property

Upon arrival N/A N/A N/A N/A

LS2.5.6 Work Time Policy Review 8715.3

AFSPCMAN 91-

Review to ensure compliance with KSC and AF regulations

Upon arrival 09.Oct.2020

LS2.5.7 Submit permits for welding/hot work (if needed) at NASA Facilities

KNPR 8715.3 Approval to perform welding/hot work on site

1 week prior to need N/A N/A N/A N/A

LS3 Launch Site Access and Accommodations

LS3.1 Submit foreign national access documentation

For VAFB and Commercial Facility access

a. Submit personnel badging information

NPR 1600.1

30SW 31-101

Approval Email/Access List

KSC - 45 days prior to arrival

VAFB - 30 days prior to arrival

Commercial - 30 days prior to arrival

09.Sep.2020 N/A

LS3.2 Submit personnel badging information

NPR 1600.1

30SW 31-101

Facility Security Manual

Approval Email/Badge 5 days prior to arrival 04.Oct.2020

LS3.3 Submit Personnel Deployment Plan

Payload Specific Approved plan 90 days prior to arrival

11.Jul.2020 N/A

LS3.4 Maintain Solvent Tracking Log LSP-UG-332.01

LSP-UG-332.02

KNPR 8500.1

Compliance with Environmental

Regulations

Upon arrival 09.Oct.2020

March 2019

Table 3.1 Launch Site Deliverables (Cont’d)

VAFB Arrival: 9 Oct 2020 Launch: 15 Dec 2020 Revised: 25 Mar 2019

Item # Item Source

Requirement for Item

Launch Site Response to Item

Submittal Requirements and

Delivery Requirements

Need Date Landsat 9 Submittal

Date

LV

Submitta l Date Status

LS3.5 Submit Personnel Medical Certifications for crane operators

LSP-UG-332.01

LSP-UG-332.02

Facility Safety

Manual

Approval to operate/handle appropriate equipment

30 days prior to arrival

09.Sep.2020

LS3.6 Submit Personnel Training Class Request(s)

LSP-UG-332.01

LSP-UG-332.02

Training class provided 30 days prior to need date

09.Sep.2020

LS3.7 Submit Camera Pass Request

- Foreign Nationals at VAF

NPG 1620.1

30SW 31-101

Approved use of cameras

3 weeks prior to need 18.Sep.2020 N/A

LS4 ELV Payload Safety Program

LS4.1 Provide Payload Safety Introduction to NASA and Range Safety (this can be held in conjunction with the Mission Concept Briefing)

a. Identify applicable safety requirements documents, tailoring assumptions and issues

b. Submit Draft Systems Safety Plan

c. Identify known spacecraft/payload systems and a preliminary assessment of potential hazards in a Preliminary hazard List

d. Present a high level Ground Operations Flow overview

e. Overview of the Mishap Preparedness and Contingency Plan (MPCP)

AFSPCM 91-710

NPR 8715.7

Deliverable direction, tailoring direction

No later than midpoint of the Preliminary

Design Phase, Phase B per NPR 7120.5

Typically 36-48 months prior to launch

Electronic to Portal Web site

31.Dec.2017 09.May.2017 N/A Closed

March 2019

Table 3.1 Launch Site Deliverables (Cont’d)

VAFB Arrival: 9 Oct 2020 Launch: 15 Dec 2020 Revised: 25 Mar 2019

Item # Item Source

Requirement for Item

Launch Site Response to Item

Submittal Requirements and

Delivery Requirements

Need Date Landsat 9 Submittal

Date

LV

Submitta l Date Status

LS4.2 Submit Safety Review I Data AFSPCM 91-710

NPR 8715.7

Approval of SSPP

Assessment of safety effort and identification of safety concerns to support KDP C

Payload PDR input

No later than 30 days prior to PDR meeting or as necessary ensuring PSWG's timely input to Key

Decision Point C per

NPR 7120.5

Typically 24-48 months prior to launch

Electronic to Portal Web site

26.Dec.2018 05.Jul.2017 N/A Closed

LS4.3 Submit Safety Review II Data

a. Preliminary MSPSP Addendum

b. Preliminary Ground Operations Plan

AFSPCM 91-710

NPR 8715.7

Approval of Final Tailored Payload Safety

Requirements

Assessment of safety effort and identification of safety concerns to support KDP D

Payload CDR input

No later than 30 days prior the project's

CDR or as necessary ensuring PSWG's timely input to Key

Decision Point D as defined in NPR

7120.5

Typically 24-27 months prior to launch

Electronic to Portal Web site

26.Dec.2018 12.Mar.2018 N/A Closed

March 2019

Table 3.1 Launch Site Deliverables (Cont’d)

VAFB Arrival: 9 Oct 2020 Launch: 15 Dec 2020 Revised: 25 Mar 2019

Item # Item Source

Requirement for Item

Launch Site Response to Item

Submittal Requirements and

Delivery Requirements

Need Date Landsat 9 Submittal

Date

LV

Submitta l Date Status

LS4.4 Submit Safety Review III Data

a. Final MSPSP Addendum

b. Final Ground Operations Plan

AFSPCM 91-710

NPR 8715.7

VAFB - Range Safety Launch Operations

Approval Letter

CCAFS - 45SW

Safety's "GO" at LRR constitutes approval;

however, a launch operations approval letter can be requested by the user if desired

No later than 60 days prior to Safety Review

III and finalized no later than 30 days before hardware shipment to the processing site

Typically 30 days prior to S/C shipment

Electronic to Portal Web site

09.Sep.2020 N/A

LS4.5 Submit Safety Verification Tracking Log (SVTL)

AFSPCM 91-710

NPR 8715.7

VAFB - Range Safety Launch Operations

Approval Letter

CCAFS - 45SW

Safety's "GO" at LRR constitutes approval;

however, a launch operations approval letter can be requested by the user if desired

Weekly upon arrival at the launch site

Electronic to Portal Web site

09.Oct.2020 N/A

LS5 Mishap Preparedness

LS5.1 Provide Launch Day Mishap Debris Team POC

NPR 8621.1B Approved MPCP 45 days prior to launch

31.Oct.2020 N/A

LS5.2 Provide SC ordnance closeout photos and photos of SC hazardous components

AFSPCM 91-710 Range debris recovery planning

30 days prior to arrival on AF property

09.Sep.2020 N/A

March 2019

Table 3.2 Observatory EGSE and MGSE List (TBR)

March 2019

Table 3.2 Observatory EGSE and MGSE List (TBR) (Cont’d)

March 2019

March 2019

March 2019

March 2019

March 2019

March 2019

March 2019

March 2019

Table 3.3 LSC (ULA) EGSE and MGSE List

Equipment Location Size (LxWxH”) Weight Power Requirements

Spacecraft Transportation Vehicle (STV), 55-87576 Seismic restraint requirements:

Eight inserts to tie down the STV/SV.

Inserts shall be 3/4"-10 UNC by 1.50" long minimum female thread and have load capability of HILTI Corp "HIS" insert part number 258023 or equivalent.

Location to be provided later.

Integration Area 17.’3” W x 46’ H No power required

Square Tube Torus ,55-87520 / 55-87565 Integration Area 235”L x 228” W x 95”H (torus supported by

STV)

No power required Notes: Dimensions include 9” added for winch handles and 5” added for top brackets. Torus height without STV support is 70.5”

Torus Handling Carts (2 Each), 55-87580 Seismic restraint requirements:

Twelve inserts for the two Torus half carts (6 per half cart).

Inserts shall be 1/2"-13 UNC by 1.12" long minimum female thread and have load capability of HILTI Corp "HIS" insert part number 258021 or equivalent.

Location to be provided later.

Integration Area 135” L x 226” W x 78” H per cart

No power required Note: without Torus installed

53ft GSE Trailer Outside, but adjacent to PPF

53ft long No external power required

Payload Mate Fixture (PMF), 55-87582 Integration Area 104.9” W x 105.3” L x 40.0 H

No power required Note: Excluding seismic tie-down turnbuckles. Max height per note 25

JLG High lifts (2 each), E450AJ Integration area 5’-9” W x 21’2” L x 6’7” stowed H

14400 lb 120VDC NEMA 5-15

March 2019

Table 3.3 LSC (ULA) EGSE and MGSE List (Cont’d)

Equipment Location Size (LxWxH”) Weight Power Requirements

Payload Fairing (PLF) Turnover Carts (2 each), 55-87507 Integration Area 180.5L x 65.0 W x

64.1 H

No power required

Hoist Beams No power required

Slings – Torus handling, 55-87577 (-3) Integration area 174” L x 174” W x

378.8 H

No power required Note: In use height: 378.8”, Storage height: 34.75”

Work Stands No Power required

March 2019

SUPPORT REQUIREMENTS AND COMM MATRIX

The following Support Requirements Matrix contains items needed to meet the requirements of the payload customer, the LSC, and the launch site team in order to implement a successful launch site flow for Landsat 9.

NOTE: General support requirements will be assigned numbers from 0001 to 9999 and located in Table 4.1. Communications and Telemetry (COMM) requirements will be assigned numbers from 10000 to 99999 and are located in Table 4.2.

MATRIX KEY FORMAT

Category (CAT) Number Range Category 0001 – 0099 Dimensions 0100 – 0199 Power/Electrical 0200 – 0299 Environment 0300 – 0399 Equipment 0400 – 0499 Furnishings 0500 – 0599 Commodities (Gasses & Liquids) 0600 – 0699 Consumables & Garments 0700 – 0799 Safety/Security 0800 – 0899 MISC Support (NASA/VAFB Range) 0900 – 0999 Mission Unique

Location (LOC) Number Range Location (LOC) 0001-0999 Payload Processing Facility Control Room (PPF CNT RM)

1000-1999 Payload Processing Facility Air Lock (PPF AL) 2000-2999 Payload Processing Facility Cleanroom (PPF CLN RM) 3000-3999 Fueling (Fueling) 4000-4999 LSC Requirements in Payload Processing Facility (PPF LSC) 5000-5999 Payload Processing Facility Miscellaneous (PPF MISC) 6000-6999 Payload Processing Facility Office Areas (PPF OFFICE) 7000-7999 Pad (PAD) 8000-8999 Building 836 (B836) 9000-9999 Other — Non-Facility Specific (OTHER)

10000 + Communication (COMM)

March 2019

0001 – 0999 PPF Control Room (PPF CNT RM) 3000-3999 Fueling (Fueling) 0001 – 0099 Dimensions 3001 – 3099 Dimensions 0100 – 0199 Power/Electrical 3100 – 3199 Power/Electrical 0200 – 0299 Environment 3200 – 3299 Environment 0300 – 0399 Equipment 3300 – 3399 Equipment 0400 – 0499 Furnishings 3400 – 3499 Furnishings 0500 – 0599 Commodities (Gasses & Liquids) 3500 – 3599 Commodities (Gasses & Liquids) 0600 – 0699 Consumables & Garments 3600 – 3699 Consumables & Garments 0700 – 0799 Safety/Security 3700 – 3799 Safety/Security 0800 – 0899 MISC Support (NASA/VAFB Range) 3800 – 3899 MISC Support (NASA/VAFB Range) 0900 – 0999 Mission Unique 3900 – 3999 Mission Unique

1000-1999 PPF Air Lock (PPF AL) 4000-4999 LSC Requirements in PPF (PPF LSC) 1001 – 1099 Dimensions 4001 – 4099 Dimensions 1100 – 1199 Power/Electrical 4100 – 4199 Power/Electrical 1200 – 1299 Environment 4200 – 4299 Environment 1300 – 1399 Equipment 4300 – 4399 Equipment 1400 – 1499 Furnishings 4400 – 4499 Furnishings 1500 – 1599 Commodities (Gasses & Liquids) 4500 – 4599 Commodities (Gasses & Liquids) 1600 – 1699 Consumables & Garments 4600 – 4699 Consumables & Garments 1700 – 1799 Safety/Security 4700 – 4799 Safety/Security 1800 – 1899 MISC Support (NASA/VAFB Range) 4800 – 4899 MISC Support (NASA/VAFB Range) 1900 – 1999 Mission Unique 4900 – 4999 Mission Unique

2000-2999 PPF Cleanroom (PPF CLN RM) 5000-5999 PPF Miscellaneous (PPF MISC) 2001 – 2099 Dimensions 5001 – 5099 Dimensions 2100 – 2199 Power/Electrical 5100 – 5199 Power/Electrical 2200 – 2299 Environment 5200 – 5299 Environment 2300 – 2399 Equipment 5300 – 5399 Equipment 2400 – 2499 Furnishings 5400 – 5499 Furnishings 2500 – 2599 Commodities (Gasses & Liquids) 5500 – 5599 Commodities (Gasses & Liquids) 2600 – 2699 Consumables & Garments 5600 – 5699 Consumables & Garments 2700 – 2799 Safety/Security 5700 – 5799 Safety/Security 2800 – 2899 MISC Support (NASA/VAFB Range) 5800 – 5899 MISC Support (NASA/VAFB Range) 2900 – 2999 Mission Unique 5900 – 5999 Mission Unique

March 2019

6000 – 6999 PPF Offline Areas (PPF OFFICE) 9000-9999 Other – Non-Facility Specific (OTHER) 6001 – 6099 Dimensions 9001 – 9099 Dimensions 6100 – 6199 Power/Electrical 9100 – 9199 Power/Electrical 6200 – 6299 Environment 9200 – 9299 Environment 6300 – 6399 Equipment 9300 – 9399 Equipment 6400 – 6499 Furnishings 9400 – 9499 Furnishings 6500 – 6599 Commodities (Gasses & Liquids) 9500 – 9599 Commodities (Gasses & Liquids) 6600 – 6699 Consumables & Garments 9600 – 9699 Consumables…