FA8818-13-R-0021_LSMA_SecL_A_FINAL.pdf

UNCLASSIFIED

Section L

APPENDIX A

MISSION INFORMATION DOCUMENTS (MIDs)

Sample Mission 2.1

PAP MCS Demo New Launch System

Mission Information Document (MID)

FA8818-13-R-0021

1.0 INTRODUCTION

1.1 OVERVIEW

1.2 PURPOSE

2.0 MISSION OBJECTIVES

3.0 ROLES AND RESPONSIBILITIES

3.1 CUSTOMER:

3.2 SMC/SDL:

3.3 MISSION ASSURANCE CONTRACTOR (MAC):

3.4 LAUNCH SYSTEM CONTRACTOR (LSC):

3.5 DEMO SYSTEMS ENGINEER CONTRACTOR (SEC):

3.6 AGREEMENTS

4.0 MISSION MILESTONE SCHEDULE

5.0 MISSION ASSURANCE REQUIREMENTS

5.1 LSMA PWS MA REQUIREMENTS

6.0 REFERENCES

1.0 INTRODUCTION

1.1 OVERVIEW

This Mission Information Document (MID) provides the mission assurance information for the Sounding Rocket Program 3 (SRP-3) contract development and launch of a demonstration launch vehicle for the Propulsion Applications Program (PAP) Medium Class System (MCS). PAP MCS Demo is sponsored by the Air Force Nuclear Warfare Center. The US Air Force, Space and Missile Systems Center (SMC) Rocket Systems Launch Program (RSLP) office, Space Development and Test Directorate (SD)/Launch Systems Division (SDL), will provide the Launch Vehicle (LV) and launch services for the SM-2.1 mission through the SRP-3 contract. The Navy will be responsible for coordination of the Space Vehicle (SV) activities.

The baseline launch location for this mission will be from Vandenberg AFB TP-01 launch site.

This is planned to be a Mission Assurance (MA) Category 2 mission, with launch system certified flightworthy by SMC/CC.

There is currently no payload for this mission.

1.2 PURPOSE

The purpose of this document is to provide mission-specific information for the SM-2.1 mission assurance effort by identifying the Launch Service Mission Assurance (LSMA) contract Performance Work Statement scope specific to this mission, and to provide schedule and other mission information required in order to propose and execute Independent Verification and Validation (IV&V) activities. This MID will:

a. Identify the overall mission objectives.

b. Identify roles and responsibilities and interfaces of which the mission assurance contractor (MAC) should be aware among the various contractors and Government agencies supporting the mission.

c. Identify the baseline mission execution schedule milestones.

d. Identify any mission-unique launch activities.

2.0 MISSION OBJECTIVES

The primary goal of the SM-2.1 mission is to demonstrate the new PAP MCS first, second, and third stage motors in an integrated system, to support a future conventional or nuclear weapon system development with flight-proven motors.

3.0 ROLES AND RESPONSIBILITIES

The roles and responsibilities among agencies and contractors that will support the SM-

2.1 mission are described below.

3.1 Customer:

The AFNWC is RSLP’s reimbursable customer for the PAP MCS Demo mission. The Customer’s Associated Contractors (ASCONs) ATK Corp, and Aerojet Inc, are responsible for manufacturing and testing the flight motors as well as supporting integration procedures.

3.2 SMC/SDL:

SMC/SD, located at Kirtland AFB, NM, is responsible for launch services including range support, LV integration, SV interface and mating, and launch services. Within SMC/SD, SDL is the division for Research and Development (R&D) and Space launch missions and is responsible for the SRP-3 launch systems and launch operations.

3.3 Mission Assurance Contractor (MAC):

The MAC provides MA and Independent Verification and Validation support to the mission in accordance with this MID.

3.4 Launch System Contractor (LSC):

SMC/SDL will contract with the LSC to provide the LV design, integration, and interface to the PAP MCS motors, mission planning and launch of the LV.

3.5 Demo Systems Engineer Contractor (SEC):

TASC is currently providing SEC services to PAP MCS Demo, including the development of motor specifications and Demo LV requirements documents.

3.6 Agreements

The MAC shall ensure that Associate Contractor Agreements are completed for the following associate contractors:

• LSC

• Tecolote Research, Inc

• Aero Thermo Technology, Inc

• MCR Federal, LLC

• TASC

• ASCONs

If necessary, the MAC shall also ensure that Non-Disclosure Agreements are completed for the above contractors.

4.0 MISSION MILESTONE SCHEDULE

The following schedule is provided for MAC proposal and planning purposes.

SRP-3 Demo Task Order RFP 15 Jan 2014 SRP-3 Demo Task Order Award 15 May 2014 Demo SRR 10 Jul 2014 Demo PDR 15 Sep 2014 Demo CDR 10 Apr 2015 Demo PSRR 15 Jan 2016 SDL MRR 30 Apr 2016 SMC FRR 1 Jun 2016 ILC 15 Aug 2017

5.0 MISSION ASSURANCE REQUIREMENTS

5.1 LSMA PWS MA Requirements

The MAC shall provide Cat2 MA (PWS Section 3.2.2) for this mission.

The TP-01 launch site at VAFB is under development to support the PAP MCS Demo.

The Period of Performance of this effort is estimated to be Apr 2014 thru Oct 2017.

6.0 REFERENCES

The following documents are included by reference for additional requirement details as specified herein.

LSMA Performance Work Statement

These documents are included in the bidder’s library for reference.

SRP-3 Contract PWS, 30 Nov 2009

CONOPS Plan for Demo Flight Test Program, PAP MCS, 12 Dec 2012

Sample Mission 2.2

MRBM-T1/T2

New Launch System

1.0 INTRODUCTION

1.1 OVERVIEW

1.2 PURPOSE

2.0 MISSION OBJECTIVES

3.0 ROLES AND RESPONSIBILITIES

3.1 CUSTOMER:

3.2 GFE MOTOR PROVIDER:

3.3 MISSION ASSURANCE CONTRACTOR (MAC):

3.4 LAUNCH SERVICES CONTRACTOR (LSC):

3.5 AGREEMENTS

4.0 MISSION MILESTONE SCHEDULE

5.0 MISSION ASSURANCE REQUIREMENTS

5.1 LSMA PWS MA REQUIREMENTS

6.0 REFERENCES

1.0 INTRODUCTION

1.1 OVERVIEW

This Mission Information Document (MID) provides the mission assurance requirements for a “Construct 2” MRBM-T1/T2 target system procured by the Missile Defense Agency (MDA). The US Air Force, Space and Missile Systems Center (SMC) Rocket Systems Launch Program (RSLP) office, Space Development and Test Directorate (SD)/Launch Systems Division (SDL), will provide the motors for the SM-2.2 mission. MDA is responsible for mission and Launch Vehicle (LV) integration activities.

The baseline launch location for this mission is TBD.

The LSC is responsible for integration of one payload with the LV. The target payload for this mission is CLASSIFIED.

1.2 PURPOSE

The purpose of this document is to provide mission-specific information for the SM-2.2 mission assurance effort by identifying the Launch Service Mission Assurance (LSMA) contract Performance Work Statement scope specific to this mission, and to provide

Independent Verification and Validation (IV&V) Construct 2 activities. This MID will:

a. Identify RSLP mission objectives.

The primary goal of RSLP’s support to the SM-2.2 mission is to support the launch an MRBM-T1/T2 target missile to meet MDA test requirements by providing certified processed motors to MDA and ensuring motor safety/certification through MDA processing and launch activities.

3.0 ROLES AND RESPONSIBILITIES

The roles and responsibilities among agencies and contractors that will support the SM-

2.2 mission are described below.

3.1 Customer:

The MDA Targets and Countermeasures Program, located in Huntsville Alabama, has a liaison at Kirtland AFB, New Mexico for motor processing. MDA identifies motor requirements and provides funding to support motor processing and system engineering. MDA technical support contractor is Aerospace Corporation.

3.2 GFE Motor Provider:

SMC/SD, located at Kirtland AFB, NM, is responsible for providing flightworthy motors for the mission in accordance with Construct 2 of the Memorandum of Agreement between SMC and MDA. Within SMC/SD, SDL is the division for Research and Development (R&D) and Space launch missions and is responsible for motor processing, safety, and certification. SDL has an operating location at Hill AFB, Utah where the motors are processed.

The MAC provides Independent Verification and Validation Construct 2 support to SMC/SD in accordance with this MARD.

3.4 Launch Services Contractor (LSC):

MDA has contracted with TBD to provide the target design, integration, vehicle mating, mission planning and launch of the target.

3.5 Agreements

The MAC shall ensure that Associate Contractor Agreements are completed for the following associate contractors:

• LSC

• Tecolote Research, Inc

• Aero Thermo Technology, Inc

• MCR Federal, LLC

Target RFP Complete Target Contract Award Oct 2013 Target SRR Jun 2014 Target PDR Oct 2014 Target MDR-2 Feb 2015 SDL Motor Buyoff #1 Jun 2015 Target #1 PSRR Mar2016 SMC Motor Certification #1 Jun 2016 ILC #1 Apr 2016 Launch Event #1 TBD

The MAC shall provide Construct 2 support (PWS 3.2.4) and GFE Flight Motor Processing (PWS 3.2.5) to one MRBM-T1/T2 mission.

The MAC shall provide GFE Ground Test Motor Processing (PWS 3.2.6) for LSC developmental testing, RCS characterization, and LSC flight hardware verification testing.

For planning and pricing purposes, the following activity is planned relevant to the GFP motors:

o Weekly GFI/GFX telecon with total of 40 GFI and 25 GFX requests o Bi-weekly motor processing telecon o Two motor processing TIMs for each mission o One motor TIM for each design review o Four weeks observe on-site LSC motor activities o Two weeks observe launch site motor activities o Two launch rehearsals and two launch attempts

The Period of Performance of this effort is estimated to be Apr 2014 thru Aug 2016.

SR19-M Rocket Motor User Handbook, 26 Apr 2013

Sample Mission 3.1

ORS-2

Existing Launch System

Mission Information Document (MID)

FA8818-13-R-0021

1.0 INTRODUCTION

1.1 OVERVIEW

1.1 PURPOSE

2.0 MISSION OBJECTIVES

3.0 ROLES AND RESPONSIBILITIES

3.1 CUSTOMER:

3.2 SMC/SDL:

3.3 MISSION ASSURANCE CONTRACTOR (MAC):

3.4 LAUNCH SERVICES CONTRACTOR (LSC):

3.5 AGREEMENTS

4.0 MISSION MILESTONE SCHEDULE

5.0 MISSION ASSURANCE REQUIREMENTS

5.1 LSMA PWS MA REQUIREMENTS

6.0 REFERENCES

1.0 INTRODUCTION

1.1 OVERVIEW

This Mission Information Document (MID) provides the mission assurance information for the Orbital Suborbital Program–3 (OSP-3) Lane 1 contract launch of a satellite on an existing design Minotaur IV launch vehicle. SM-3.1 is a space launch mission being sponsored by the Operationally Responsive Space (ORS) Office. The US Air Force, Space and Missile Systems Center (SMC) Rocket Systems Launch Program (RSLP) office, Space Development and Test Directorate (SD)/Launch Systems Division (SDL), will provide the Launch Vehicle (LV) and launch services for the SM-3.1 mission through the OSP-3 contract. ORS will be responsible for coordination of the Space Vehicle (SV) activities.

The baseline launch location for this mission will be from the Mid-Atlantic Regional Spaceport (MARS) on Wallops Island.

The LSC is responsible for integration of one space vehicle with the LV. The payload for this mission is UNCLASSIFIED.

1.1 PURPOSE

The purpose of this document is to provide mission-specific information for the SM-3.1 mission assurance effort by identifying the Launch Service Mission Assurance (LSMA) contract Performance Work Statement scope specific to this mission, and to provide

The primary goal of the SM-3.1 mission is to launch a 3,000 lb SV with radar sensor into a 311 km circular LEO orbit at 45 degrees inclination.

The SV will be launched into orbit by the LV, and has no onboard propulsion. The SM-

3.1 SV will separate from the LV via a SV provided motorized lightband separation system. Following the separation event, the LV will perform a Collision/Contamination

Avoidance Maneuver (C/CAM) to minimize contamination and potential recontact with the SV, and will either move into an allowed orbit or be de-orbited to meet space debris requirements.

3.0 ROLES AND RESPONSIBILITIES

The roles and responsibilities among agencies and contractors that will support the SM-

3.1 mission are described below.

3.1 Customer:

The SV is being provided to RSLP by the ORS Office. The Customer Space Vehicle Contractor (SVC) is responsible for manufacturing and testing the SV as well as supporting joint LV/SV integration procedures.

range support, LV integration, SV interface and mating, and launch services. Within missions and is responsible for the OSP-3 launch services.

SMC/SDL contracted with TBD to provide the LV design, integration, and interface to the SV, vehicle mating, mission planning and launch of the LV.

following associate contractors:

• LSC

• Tecolote Research, Inc

Launch Service Task Order RFP 1 Jun 2014 Launch Service Task Order Award 1 Oct 2014 LSC SRR 10 Dec 2014 LSC MDR-1 15 Jul 2015 LSC MDR-2 10 Dec 2015 LSC PSRR 15 Apr 2016 SDL MRR 30 Apr 2016 SMC FRR 5 Jul 2016 ILC 15 Jul 2016

The MAC shall provide Cat1 MA (PWS Section 3.2.1) for this mission.

The MAC shall provide GFE motor refurbishment (PWS Section 3.2.5) for this mission.

The Period of Performance of this effort is estimated to be Apr 2014 thru Oct 2016.

6.0 REFERENCES

Minotaur IV, V, VI User’s Guide, Release 2.0, Mar 2013

Minotaur I User’s Guide, Release 2.1, Jan 2006

Athena Launch Service User’s Guide, 15 Apr 2013

Sample Mission 3.2

STP-3

Mission Information Document (MID)

FA8818-13-R-0021

1.0 INTRODUCTION

1.1 OVERVIEW

1.2 PURPOSE

2.0 MISSION OBJECTIVES

3.0 ROLES AND RESPONSIBILITIES

3.1 CUSTOMER:

3.2 SMC/SDL:

3.3 MISSION ASSURANCE CONTRACTOR (MAC):

3.4 LAUNCH SERVICES CONTRACTOR (LSC):

3.5 AGREEMENTS

4.0 MISSION MILESTONE SCHEDULE

5.0 MISSION ASSURANCE REQUIREMENTS

5.1 LSMA PWS MA REQUIREMENTS

6.0 REFERENCES

1.0 INTRODUCTION

1.1 OVERVIEW

This Mission Information Document (MID) provides the mission assurance information for the Orbital Suborbital Program–3 (OSP-3) Lane 2 contract launch of a developmental satellite on an existing design launch vehicle. SM-3.2 is a space launch mission being sponsored by the Space Test Program (STP). The US Air Force, Space and Missile Systems Center (SMC) Rocket Systems Launch Program (RSLP) office, Space Development and Test Directorate (SD)/Launch Systems Division (SDL), will provide the Launch Vehicle (LV) and launch services for the SM-3.2 mission through the OSP-3 contract. STP will be responsible for coordination of the Space Vehicle (SV) activities.

The baseline launch location for this mission will be determined at contract award.

The LSC is responsible for integration of six payloads (one primary and five secondaries) with the LV. The payloads for this mission are UNCLASSIFIED.

1.2 PURPOSE

The purpose of this document is to provide mission-specific information for the SM-3.2 mission assurance effort by identifying the Launch Service Mission Assurance (LSMA) contract Performance Work Statement scope specific to this mission, and to provide

The primary goal of the SM-3.2 mission is to integrate and launch six payloads into TBD orbit(s) to meet STP objectives. A secondary objective of the mission is to demonstrate an EELV New Entrant.

The SV will be launched into orbit by the LV, and has onboard propulsion for some portions of the IPS. The SM-3.2 payloads will separate from the LV via LV-provided separation systems. Following the separation event, the LV will perform a

Collision/Contamination Avoidance Maneuver (C/CAM) to minimize contamination and potential recontact with the SV, and will either move into an allowed orbit or be de-orbited to meet space debris requirements.

3.0 ROLES AND RESPONSIBILITIES

The roles and responsibilities among agencies and contractors that will support the SM-

3.2 mission are described below.

3.1 Customer:

The SV is being provided to RSLP by STP. STP’s Space Vehicle Contractors (SVCs) are responsible for manufacturing and testing the payloads, as well as supporting joint LV/SV integration procedures, but the LV provider will integrate the payloads onto LV-provided multiple payload adapter(s). Additionally, STP will provide submissions for the LSC’s Range Safety documentation at the request of SMC/SDL.

range support, LV integration, SV interface and mating, and launch services. Within missions and is responsible for the OSP-3 launch systems and launch operations.

SMC/SDL contracted with the LSC to provide the LV design, integration, and interface to the SV, vehicle mating, mission planning and launch of the LV.

following associate contractors:

• LSC

• Tecolote Research, Inc

Launch Service Task Order RFP 1 Sep 2017 Launch Service Task Order Award 1 Jan 2018 LSC SRR 10 Jun 2018 LSC MDR-1 15 Dec 2018 LSC MDR-2 10 Jul 2019 LSC PSRR 15 Apr 2020 SDL MRR 30 Apr 2020 SMC FRR 5 Jun 2020 ILC 15 Jun 2020

The MAC shall provide Cat2 MA (PWS 3.2.2) for this mission.

The Period of Performance of this effort is estimated to be Aug 2017 thru Sep 2020.

Minotaur IV, V, VI User’s Guide, Release 2.0, Mar 2013

Antares OSP-3 User’s Guide, Draft Release 1.0, Mar 2013

Falcon 9 Launch Vehicle Payload User’s Guide, Revision 2

Falcon Heavy Launch Vehicle Payload User’s Guide, Revision 0

Sample Mission 3.3

Navsat Launch Service

1.0 INTRODUCTION

1.1 OVERVIEW

1.2 PURPOSE

2.0 MISSION OBJECTIVES

3.0 ROLES AND RESPONSIBILITIES

3.1 CUSTOMER:

3.2 SMC/SDL:

3.3 MISSION ASSURANCE CONTRACTOR (MAC):

3.4 LAUNCH SERVICES CONTRACTOR (LSC):

3.5 AGREEMENTS

4.0 MISSION MILESTONE SCHEDULE

5.0 MISSION ASSURANCE REQUIREMENTS

5.1 LSMA PWS MA REQUIREMENTS

6.0 REFERENCES

1.0 INTRODUCTION

1.1 OVERVIEW

This Mission Information Document (MID) provides the mission assurance information for the Orbital Suborbital Program–3 (OSP-3) Lane 2 contract launch of a pair of navigational satellites on an existing design Falcon Heavy launch vehicle. SM-3.3 is a space launch mission being sponsored by SMC. The US Air Force, Space and Missile Systems Center (SMC) Rocket Systems Launch Program (RSLP) office, Space Development and Test Directorate (SD)/Launch Systems Division (SDL), will provide the Launch Vehicle (LV) and launch services for the SM-3.3 mission through the OSP-3 contract. SMC will be responsible for coordination of the Space Vehicle (SV) activities.

The baseline launch location for this mission will be from the Cape Canaveral Air Force Station.

The LSC is responsible for integration of two space vehicles with the LV. The payload for this mission is UNCLASSIFIED.

1.2 PURPOSE

The purpose of this document is to provide mission-specific information for the SM-3.3 mission assurance effort by identifying the Launch Service Mission Assurance (LSMA) contract Performance Work Statement scope specific to this mission, and to provide

The primary goal of the SM-3.3 mission is to launch two 1100 kg SVs with navigational payloads via direct injection into a 20,300 km MEO with 55 degrees inclination.

The SM-3.3 SVs will separate from the LV via an LV-provided separation system.

Following the separation events, the LV will perform a Collision/Contamination Avoidance Maneuver (C/CAM) to minimize contamination and potential recontact with the SVs, and will either move into an allowed orbit or be de-orbited to meet space debris requirements.

3.3 mission are described below.

3.1 Customer:

The SV is being provided to RSLP by an SMC SPO. The Customer Space Vehicle Contractor (SVC) is responsible for manufacturing and testing the SVs as well as supporting joint LV/SV integration procedures. Additionally, the SV System Program Office (SPO) will provide submissions for the LSC’s Range Safety documentation at the request of SMC/SDL.

range support, LV integration, SV interface and mating, and launch services. Within following associate contractors:

• LSC

• Tecolote Research, Inc

Launch Service Task Order RFP 1 Feb 2015 Launch Service Task Order Award 1 Jun 2015 LSC SRR 10 Sep 2015 LSC MDR-1 15 Jan 2016 LSC MDR-2 10 Dec 2016 LSC PSRR 15 Feb 2017 SDL MRR 30 Apr 2017 SMC FRR 5 Jun 2017 ILC 15 Jun 2017

The MAC shall provide Cat3 MA (PWS Section 3.2.3) for this mission.

The Period of Performance of this effort is estimated to be Jan 2015 thru Sep 2017.

6.0 REFERENCES

Sample Mission 3.4

Navsat2 Launch Service

1.0 INTRODUCTION

1.1 OVERVIEW

1.1 PURPOSE

2.0 MISSION OBJECTIVES

3.0 ROLES AND RESPONSIBILITIES

3.1 CUSTOMER:

3.2 SMC/SDL:

3.3 MISSION ASSURANCE CONTRACTOR (MAC):

3.4 LAUNCH SERVICES CONTRACTOR (LSC):

3.5 AGREEMENTS

4.0 MISSION MILESTONE SCHEDULE

5.0 MISSION ASSURANCE REQUIREMENTS

5.1 LSMA PWS MA REQUIREMENTS

6.0 REFERENCES

1.0 INTRODUCTION

1.1 OVERVIEW

This Mission Information Document (MID) provides the mission assurance information for the Orbital Suborbital Program–3 (OSP-3) Lane 2 contract launch of a pair of navigational satellites on an existing design Falcon Heavy launch vehicle. SM-3.4 is a space launch mission being sponsored by SMC. The US Air Force, Space and Missile Systems Center (SMC) Rocket Systems Launch Program (RSLP) office, Space Development and Test Directorate (SD)/Launch Systems Division (SDL), will provide the Launch Vehicle (LV) and launch services for the SM-3.4 mission through the OSP-3 contract. SMC will be responsible for coordination of the Space Vehicle (SV) activities.

The baseline launch location for this mission will be from the Cape Canaveral Air Force Station.

The LSC is responsible for integration of two space vehicles with the LV. The payload for this mission is UNCLASSIFIED.

1.1 PURPOSE

The purpose of this document is to provide mission-specific information for the SM-3.4 mission assurance effort by identifying the Launch Service Mission Assurance (LSMA) contract Performance Work Statement scope specific to this mission, and to provide

The primary goal of the SM-3.4 mission is to launch two 1100 kg SVs with navigational payloads via direct injection into a 20,300 km MEO with 55 degrees inclination.

The SM-3.4 SVs will separate from the LV via an LV-provided separation system.

Following the separation events, the LV will perform a Collision/Contamination Avoidance Maneuver (C/CAM) to minimize contamination and potential recontact with the SVs, and will either move into an allowed orbit or be de-orbited to meet space debris requirements.

3.4 mission are described below.

3.1 Customer:

The SV is being provided to RSLP by an SMC SPO. The Customer Space Vehicle Contractor (SVC) is responsible for manufacturing and testing the SVs as well as supporting joint LV/SV integration procedures. Additionally, the SV System Program Office (SPO) will provide submissions for the LSC’s Range Safety documentation at the request of SMC/SDL.

range support, LV integration, SV interface and mating, and launch services. Within following associate contractors:

• LSC

• Tecolote Research, Inc

Launch Service Task Order RFP 1 Feb 2016 Launch Service Task Order Award 1 Jun 2016 LSC SRR 10 Sep 2016 LSC MDR-1 15 Jan 2017 LSC MDR-2 10 Dec 2017 LSC PSRR 15 Feb 2018 SDL MRR 30 Apr 2018 SMC FRR 5 Jun 2018 ILC 15 Jun 2018

The MAC shall provide Cat2 MA (PWS Section 3.2.2) for this mission.

The Period of Performance of this effort is estimated to be Jan 2016 thru Sep 2018.

Sample Mission 3.5 eMRBM

1.0 INTRODUCTION

1.1 OVERVIEW

1.2 PURPOSE

2.0 MISSION OBJECTIVES

3.0 ROLES AND RESPONSIBILITIES

3.1 CUSTOMER:

3.2 GFE MOTOR PROVIDER:

3.3 MISSION ASSURANCE CONTRACTOR (MAC):

3.4 LAUNCH SERVICES CONTRACTOR (LSC):

3.5 AGREEMENTS

4.0 MISSION MILESTONE SCHEDULE

5.0 MISSION ASSURANCE REQUIREMENTS

5.1 LSMA PWS MA REQUIREMENTS

6.0 REFERENCES

1.0 INTRODUCTION

1.1 OVERVIEW

This Mission Information Document (MID) provides the mission assurance requirements for a “Construct 2” eMRBM target system procured by the Missile Defense Agency (MDA). The US Air Force, Space and Missile Systems Center (SMC) Rocket Systems Launch Program (RSLP) office, Space Development and Test Directorate (SD)/Launch Systems Division (SDL), will provide the motors for the SM-3.5 mission. MDA is responsible for mission and Launch Vehicle (LV) integration activities.

The baseline C-17 deployment location for this mission is Hickam AFB, HI.

The target payload for this mission is CLASSIFIED.

1.2 PURPOSE

The purpose of this document is to provide mission-specific information for the SM-3.5 mission assurance effort by identifying the Launch Service Mission Assurance (LSMA) contract Performance Work Statement scope specific to this mission, and to provide

Independent Verification and Validation (IV&V) Construct 2 activities. This MID will:

a. Identify RSLP mission objectives.

The primary goal of RSLP’s support to the SM-3.5 mission is to support the launch an eMRBM target missile to meet MDA test requirements by providing certified processed motors to MDA and ensuring motor safety/certification through MDA processing and launch activities.

3.5 mission are described below.

3.1 Customer:

The MDA Targets and Countermeasures Program, located in Huntsville Alabama, has a liaison at Kirtland AFB, New Mexico for motor processing. MDA identifies motor requirements and provides funding to support motor processing and system engineering. MDA technical support contractor is Aerospace Corporation.

3.2 GFE Motor Provider:

SMC/SD, located at Kirtland AFB, NM, is responsible for providing flightworthy motors for the mission in accordance with Construct 2 of the Memorandum of Agreement between SMC and MDA. Within SMC/SD, SDL is the division for Research and Development (R&D) and Space launch missions and is responsible for motor processing, safety, and certification. SDL has a operating location at Hill AFB, Utah where the motors are processed.

The MAC provides Independent Verification and Validation Construct 2 support to SMC/SD in accordance with this MARD.

MDA has contracted with Lockheed Martin Space Systems Corporation (LMSSC) to provide the target design, integration, vehicle mating, mission planning and launch of the target.

following associate contractors:

• LMSSC

• Tecolote Research, Inc

• Aero Thermo Technology, Inc

• Aerospace Corp.

• TASC

4.0 MISSION MILESTONE SCHEDULE

The following schedule is provided for MAC proposal and planning purposes. The first two eMRBM targets are supported under a prior contract, not within the scope of this

MID.

Prior/Current events not covered by this MID:

Target RFP Complete Target Contract Award Complete Target SRR Complete Target PDR Complete Target MDR-2 Complete SDL Motor Buyoff #1 Complete Target #1 PSRR Complete SMC Motor Certification #1 Complete ILC #1 Complete Launch Event #1 Complete SDL Motor Buyoff #2 & #3 Aug 2014 Target #2 & #3 PSRR Feb 2015 SMC Motor Certification #2 Aug 2015 ILC #2 & #3 Apr 2015 Launch Event #2 & #3 TBD

Events covered by this MID:

Monitor LSC motor processing Oct 2014- Apr 2015 SDL Motor Buyoff #4 Jul 2015 Target #4 PSRR Feb 2016 SMC Motor Certification #4 Mar 206 ILC #4 Apr 2016 Launch Event #4 TBD

The MAC shall provide Construct 2 support (PWS 3.2.4) and GFE Flight Motor Processing (PWS 3.2.5) to one eMRBM missions.

The MAC shall provide GFE Ground Test Motor Processing (PWS 3.2.6) for LSC flight hardware verification testing.

For planning and pricing purposes, the following activity is planned to continue relevant to the eMRBM GFP motors:

o Bi-Weekly GFI/GFX telecon o Bi-weekly motor processing telecon o Two motor processing TIMs for each mission o Four weeks observe on-site LSC motor activities o Two weeks observe launch site motor activities o Two launch rehearsals and two launch attempts

The Period of Performance of this effort is estimated to be Oct 2014 thru Aug 2016.

eMRBM Baseline Requirements Document (BRD), 20 Sep 2012 eMRBM Process Order, 30 Jul 2012 eMRBM GFX-GFI list eMRBM MM Processing Schedule, 10 Aug 2012

SR19-AJ Rocket Motor User Manual, 26 Apr 2013

SR19-M Rocket Motor User Handbook, 26 Apr 2013

SMC/CC Motor Certification Readiness Review, 19 Aug 2013

6.0 REFERENCES

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6.0 REFERENCES