6.a-L102_Appendix_A__-_MID_SM-2.2_v5_4_Feb_2013.docx

UNCLASSIFIED// SM-2.2

UNCLASSIFIED

Sample Mission 2.2

Minotaur 6 New Launch System Mission Information Document (MID)

FA8818-13-R-TBD

Draft v5 4 Feb 2013

REVISION HISTORY

INTRODUCTION

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 satellite on a developmental design (PDR-level) Minotaur 6 launch vehicle. SM-2.2 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-2.2 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 Kodiak Launch Complex.

This will be an OSP-3 mission, but the Mission Assurance (MA) Category will not be determined until launch service award. The MAC should provide a single proposal including an MA Cat2 baseline, with a priced option to reduce the MA to Cat1 within 30 days of task order award.

The payload for this mission is UNCLASSIFIED.

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 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.

MISSION OBJECTIVES

The primary goal of the SM-2.2 mission is to launch an 1100 kg SV with a navigational payload into a MEO Transfer Orbit (MTO) with apogee at 20,300 km (objective) and 55 degrees inclination.

The SV will be launched into a transfer orbit by the LV, and will perform its own circularization with onboard systems. The SM-2.2 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.

ROLES AND RESPONSIBILITIES

The roles and responsibilities among agencies and contractors that will support the SM-2.2 mission are described below.

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 SV 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.

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 OSP-3 launch systems and launch operations.

Mission Assurance Contractor (MAC):

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

Launch Services Contractor (LSC):

SMC/SDL contracted with Orbital Sciences Corp via the OSP-3 contract to provide the LV design, integration, and interface to the SV, vehicle mating, mission planning and launch of the LV.

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

· LSC

· Tecolote Research, Inc

· Aero Thermo Technology, Inc

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

MISSION MILESTONE SCHEDULE

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

MISSION ASSURANCE REQUIREMENTS

LSMA PWS MA Requirements The MAC shall provide Cat2 MA (PWS Section 3.2.2) for this mission in accordance with the PWS.

The mission includes LSC conduct of a booster mechanical pathfinder at Kodiak Launch Complex approximately one year prior to the ILC, and developmental (modal) testing, which require GFE Ground Test Motor processing support (PWS Section 3.2.6).

The MAC shall also provide GFE flight motor processing support (PWS Section 3.2.5) for this mission.

The Period of Performance of this effort is estimated to be Jul 2018 thru Sep 2020.

REFERENCES

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

LSMA Performance Work Statement, dd mmm yyyy.

OSP-3 Lane 2 User’s Guide, dd mmm yyyy.

1 | UNCLASSIFIED// NOT FOR PUBLIC RELEASE

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