6.a-L102_Appendix_A__-_MID_SM-3.4_v5_4_Feb_2013.docx
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- Attached to
- Launch Services Mission Assurance (LSMA) Federal contract opportunity
- Solicitation number
- FA8818-13-R-0021
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FA8818-13-R-0021 L102 Appendix A - Sample Mission 3.4
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UNCLASSIFIED// SM-3.4
UNCLASSIFIED
Sample Mission 3.4
STP-3
Existing Launch System Mission Information Document (MID)
FA8818-13-R-TBD
Draft v5 4 Feb 2013
REVISION HISTORY
| REVISION |
| DATE |
| SECTION AFFECTED |
| COMMENTS |
| 0 |
| TBD |
| All |
| LSMA Draft RFP |
| 1.0 | INTRODUCTION | 3 |
| 1.1 | OVERVIEW | 3 |
| 1.2 | SCOPE | Error! Bookmark not defined. |
| 2.0 | MISSION OBJECTIVES | 3 |
| 3.0 | ROLES AND RESPONSIBILITIES | 4 |
| 3.1 | Customer: | 4 |
| 3.2 | SMC/SDL: | 4 |
| 3.3 | Mission Assurance Contractor (MAC): | 4 |
| 3.4 | Launch Services Contractor (LSC): | 4 |
| 3.5 | Agreements | 4 |
| 4.0 | MISSION MILESTONE SCHEDULE | 5 |
| 5.0 | MISSION ASSURANCE REQUIREMENTS | 5 |
| 5.1 | LSMA PWS MA Requirements | 5 |
| 6.0 | REFERENCES | 5 |
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 developmental satellite on an existing design launch vehicle. SM-3.4 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-3.4 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.
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 Cat1 baseline, with a priced option to increase the MA to Cat2 within 30 days of task order award.
The payload for this mission is UNCLASSIFIED.
0. 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 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-3.4 mission is to integrate and launch a TBD kg Integrated Payload Stack (IPS) SV 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-3.4 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.
ROLES AND RESPONSIBILITIES
The roles and responsibilities among agencies and contractors that will support the SM-3.4 mission are described below.
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.
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 the LSC 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.
| 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 |
MISSION ASSURANCE REQUIREMENTS
LSMA PWS MA Requirements 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.
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
LSMA SM-3.4 – Rev 0 Page 2 of 5
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