JuanCastillo29/space-mission-intelligence-data huggingface dataset:
Launch Site Integration Reviews (LSIRs)

EGS Program LSIRs have been developed to align with the payload’s milestone review schedule (PDR, CDR, etc.).  The processes build upon and apply best practices and lessons learned to reduce program and technical risk while improving mission success. Iterations of these reviews (LSIR 1-LSIR 4) will be held in parallel with external program reviews. LSIRs ensure feasibility and compatibility of the payload with EGS ground operations as the integration process matures. Prior to arrival of flight equipment for processing at KSC, all related EGS facilities, support equipment (such as GSE) and ground systems will be readied for receiving and processing flight hardware and software. Incoming support equipment (GSE) must go through an acceptance process for use at KSC.

LSIR 1 will demonstrate EGS's capability to support the Payload Customer during its processing at KSC. This will also be a review of preliminary payload requirements and Non-Standard Services (NSS). LSIR 2 will be a review of the baselined requirements and support services. LSIR 3 will serve as a review of the finalized requirements. The Baselined LSSRD will be a reviewable document and the PRD will be in development. Lastly LSIR 4 will review all finalized commitments, ensure that the PRD has been sent to suppliers, and the Final LSSRD will be available for review. LSIR 4 will ensure EGS compliance with Payload Customer requirements have been verified and any residual risks have been deemed acceptable for Customer processing at KSC.
Spacecraft/Payloads Verification Complete

After completion of the spacecraft/payload’s hardware and software build and testing, the spacecraft/payload will submit to SPIE all verification compliance deliverables, including test verified models, analysis, etc. through the DVO process. There may be cases where verification will need to remain open until after the spacecraft/payload has been shipped to KSC and fully integrated into the vehicle by EGS. The spacecraft/payload will provide a listing of any approved waivers to engineering and safety requirements. SPIE will maintain a safety verification tracking log that identifies open safety verification methods, status and expected closure.  This information will provide inputs to conduct a successful Pre-Ship Review.
The electronic version is the official approved document.

PSS Payload Separation System RH Right Hand RF Radio Frequency RFTS ROAP
Radio Frequency and Telemetry Station Removable Overhead Access Platform RSRM Reusable Solid Rocket Motor SA Spacecraft Adapter SCCS Spaceport Command and Control System sec SI SECO
Second Second Stage Engine Cut-off International System of Units SIR System Integration Review SLS SM
Space Launch System Science Mission SP Spacecraft/payload SPDS SPIR SPL
Secondary Payload Deployment System Spacecraft/Payload Integration Review Secondary Payload SPIE Spacecraft/Payload Integration & Evolution SRD System Requirements Document SRB Solid Rocket Booster SRR SRS SS
Systems Requirement Review Shock Response System Sound Suppression SSPF Space Station Processing Facility t TAIR
Metric Tons Test and Assembly Inspection Record T&CD Timing and Countdown Subsystem TLI Trans-Lunar Injection UPS Uninterruptible Power Supply USA Universal Stage Adapter VAB Vehicle Assembly Building VAC Volts Alternating Current VCF Vapor Containment Facility W Watt WAD Work Authorization Document
Flight Readiness Review (FRR)

The Flight Readiness Review (FRR) process will certify readiness for flight in the form of approved Certificate of Flight Readiness (CoFR). A sequence of CoFR reviews will be conducted prior to final rollout of SLS to the pad consisting of organizational, Element, Program and ESD Pre-FRRs which will culminate in the Agency FRR. The Agency FRR will provide a final pre-launch assessment of the integrated SLS-spacecraft/payload system and launch facility readiness, including open work and risks to the readiness of flight and ground systems, the ER and Western landing and recovery, network assets, personnel, and procedures necessary to perform launch through landing and recovery operations. The  sequence of CoFR reviews will ensure that the spacecraft/payload, SLS systems, facilities, GSE and all supporting organizations are ready and committed to support final launch preparations, countdown and launch. SPIE will represent the spacecraft/payload during this sequence of CoFR related reviews.
ACRONYMS AND ABBREVIATIONS

AC ACM
Alternating Current Access Control Monitor ADMIT AU
Accommodation Demand Model Input Template Avionics Unit BL Baseline BCDS Broadband Communication Distribution System BTU British Thermal Unit C C3 C3R CAA
Celsius Characteristic Energy (km2/s2) Command, Control, Communication and Range Crew Access Arm CAD Computer-Aided Design CCAFS Cape Canaveral Air Force Station CCTV Closed Circuit Television CDR Critical Design Review CD&SC Communications Distribution and Switching Center CG Center of gravity CM COTS
Crew Module Commercial Off The Shelf CPL Co-manifested Payload CR Change Request CT Crawler-Transporter CWA C&DHS
Clean Work Area Command and Data Handling System D Draft DCSS Delta Cryogenic Second Stage DRO Distant Retrograde Orbit DVO Detailed Verification Objective ECS Environmental Control System EELV EGS EGSE
Evolved Expendable Launch Vehicle Exploration Ground Systems Electrical Ground Support Equipment ELV Expendable Launch Vehicle EM Exploration Mission
The electronic version is the official approved document.

EMC EME
Electromagnetic Capability Electromagnetic Environment ER Eastern Range ESD Exploration Systems Development ESPA EELV Secondary Payload Adapter EUS EUSU
Exploration Upper Stage Exploration Upper Stage Umbilical F FOD FPR
Fahrenheit Flight Operations Directorate Flight Performance Reserve FR Firing Room FRR Flight Readiness Review ft Foot (Feet) ft/sec Feet per Second ft2 Square Feet ft3 Cubic Feet GCS GFAS
Ground Cooling System Ground & Flight Application Software GHe Gaseous Helium GN2 Gaseous Nitrogen GO2 Gaseous Oxygen GOR Ground Operations Review GSE Ground Support Equipment HazGas Hazardous Gas HB High Bay HEPA High-Efficiency Particulate Air HEOMD HPF HVAC
Human Exploration and Operations Mission Directorate Hazardous Processing Facility Heating, ventilation, and air conditioning (HVAC) ICD ICPS
Interface Control Document Interim Cryogenic Propulsion Stage IMLEO Injected Mass at Low Earth Orbit in Inch IOP Ignition Overpressure IRD Interface Requirements Document
Isp
Specific Impulse International Organization for Standardization
ISO
The electronic version is the official approved document.

ISPE Integrated Spacecraft and Payload Element ISS International Space Station JEL Jacking, Equalization and Leveling kg Kilogram KITS Kennedy Integrated Test System km Kilometer KNET KSC Network KSC kVA
Kennedy Space Center kilovolt amperes lbm Pounds Mass LC Launch Complex LCC LCS
Launch Commit Criteria Launch Control System LEO Low-Earth Orbit LH2 Liquid Hydrogen LOX LSIM LSIR LSP
Liquid Oxygen Launch Site Integration Manager Launch Site Integration Reviews Launch Service Program LSSRD Launch Site Support and Requirements Document LV LVSA
Launch Vehicle Launch Vehicle Stage Adapter m Meter m/s Meters per Second m3 Cubic Meters MAX Maximum MCR MDE
Mission Concept Review Mission Dependent Equipment MECO Main Engine Cut-Off MGA Mass Growth Allowance Min MIN
Minute Minimum ML Mobile Launcher MLB Mobile Launcher Base MLI Multilayer Insulation MLT MOSB
Mobile Launch Tower Mission Operations Support Building
The electronic version is the official approved document.

MPE Maximum Predicted Environment MPG Mission Planner’s Guide MPPF MPPU
Multi Payload Processing Facility Mini Portable Purge Units MSFC Marshall Space Flight Center NASA National Aeronautics and Space Administration nm Nautical Mile NRHO NSS
Near Rectilinear Halo Orbit Non Standard Service NVR Non-Volatile Residue OIS Operational Information System OML Outer Mold Line OPR Office of Primary Responsibility OMRS Operations and Maintenance Requirements Specifications OSA Orion Stage Adapter OISD Operational Intercommunication Systems-Digital OSMU Orion Service Module Umbilical OTV P
Operational Television Preliminary PAF PAS
Payload Attach Fitting Payload Accommodation Subsystem PAWS Paging and Area Warning System PDR Preliminary Design Review PHSF Payload Hazardous Servicing Facility PIA Payload Integration Agreement PIA PIM PLA
Payload Interface Adapter Payload Integration Manager Payload Adapter PLF Payload Fairing PMR Program Manager’s Reserve POCS II Photo Optical Control System II PPL PPF PRD
Primary Payload Payload Processing Facility Program Requirements Document psi Pound per square inch PSM Payload System Mass PSR Payload Safety Review
ACCOMMODATION DEMAND MODEL INPUT TEMPLATE (ADMIT) SURVEY

Completing the ADMIT survey is the first step in defining requirements, interface details, and preliminary safety data for spacecraft/payload that could be manifested on SLS. If a spacecraft/payload unique Interface Requirements Document (IRD) or equivalent already exists, it may replace an ADMIT response if the needed data is contained there.  It is understood that a specific response to some ADMIT questions may not be possible due to mission/design maturity. Other information or constraints considered pertinent by the spacecraft/payload should also be included in addition to an ADMIT response. Spacecraft/payload ADMIT survey and/or IRD responses can be submitted to NASA-slspayloads@mail.nasa.gov. A representative from the SLS SPIE office will contact you to discuss your spacecraft/payload requirements in greater detail.
Describe any deployable systems used during the ascent/on-orbit phase.  Describe any laser systems employed.  Describe any radioactive devices contained on the spacecraft/payload, including type and quantity of material.  Describe any pressure vessels employed, and their location on the spacecraft.  Describe any explosive devices installed (pyros, separation system, etc.).  Describe any unique features that may pose a hazard to crew or ground personnel or require specific processing environments or constraints (temperature, shock, vibration, or acoustic).  If the spacecraft/payload will be flying as part of a crewed mission, list any systems planned to activate prior to Orion separation.
 Describe high level Processing Facility requirements, including the planned approach for spacecraft buildup at KSC or at private facility, as well as dwell time and processing timeline. Include an Operations Flow Chart, detailed sequence of operations, and all spacecraft related launch site activities.
 Identify any hazardous processes such as fueling or ordinance installation. If fueling is involved identify the type of the fuel utilized.
 Describe any test you will need to conduct at KSC (i.e. Structural test, fit test, etc.). Specify any Ground Support Equipment that will be utilized and its electrical power needs.
The electronic version is the official approved document.

 Additional Services – Identify any other services or requirements not previously mentioned.
This could include but is not limited to sensitive security concerns that are specific to the spacecraft, power being supplied during rollout, power being supplied at VAB or Pad, power required during launch/ascent, communications/data requirements, purge requirements, thermal requirements, cleanliness requirements, unique mounting requirements, or defining any necessary post encapsulation access requirements.