Minimum Award LSUG SOW.pdf

Attachment 1 Launch Service User Guide (LSUG)

Statement of Work (SOW)

Basic: 29 July 2019

PREPARED BY

SPACE SYSTEMS CENTER

ASSURED ACCESS TO SPACE DIRECTORATE

SMALL LAUNCH AND TARGETS DIVISION

ROCKET SYSTEMS LAUNCH PROGRAM (RSLP)

KIRTLAND AFB, NM

1. SCOPE

1.1 PURPOSE: This Statement of Work (SOW) identifies Task Order 0001 – Launch Service

User Guide (LSUG) requirements under Orbital Services Program-4 (OSP-4). The LSUG provides the Government with insight into the potential performance capability of the OSP-4 contractor(s) for the purpose of informing pre-solicitation planning activities with potential

RSLP customers. Each successful Offeror will be awarded Task Order 0001 which constitutes as the guaranteed minimum amount ordered on this contract.

2. REQUIREMENTS

2.1 LAUNCH SERVICE USER GUIDE: The Offeror shall develop a LSUG which conforms to the format identified below; for any information that is currently not available, include the section and identify the missing information as “TBD”. The LSUG shall include all current

Launch Vehicle (LV) configurations at the time of publication and include these additional

LV(s) as an addendum to the LSUG. [CRDL D002]

Launch Service User Guide (LSUG) Format

Section Number

Section Information Description

1 Introduction

1.1 Overview of Company and Launch Vehicles

(LVs)

Brief overview, mission description, LV name and description, history, location of facilities

1.2 LV Reliability

Flight success history, if available, and reliability analysis data

1.3 Injection Orbits Inclination range, altitude range, LEO, GTO

1.4 Mass-to-Orbit Family of plots by orbit regime

1.5 Injection Accuracy Perigee, apogee, inclination tolerances

1.6 Separation Attitude and Accuracy Tolerances and roll/pitch/yaw rates

1.7 Launch Windows

Any restrictions or constraints on launch windows

1.8

Launch Sites Current launch sites; future launch sites in work; any restrictions or constraints on launch sites

2 Launch Vehicle(s)

2.1

LV structure and systems:

Structure and Propulsion

Separation System

Fairing Avionics/GNC

Includes stages, interstages, fairing, materials, thrust level, dimensions, propellant type (liquid or solid)

2.2 Coordinate Frame

Standard coordinate system used by the LV for PL/LV interface reference

2.3

Payload Envelope(s)

Dimensions of LV static and dynamic payload envelope(s) that provide the usable volume inside the fairing and forward of the

Standard Interface Plane (SIP) in US

Customary Units

2.4 Payload Mass Properties and Center of Gravity

The limits of Payload Mass and Center of

Gravity that the LV can accommodate.

2.5 Multiple Payload Support Adapters, support for cubesats

2.6

Mechanical Interfaces:

PL Adapters PL Fairing PL Fairing Access Doors

Includes size, bolt pattern, dimensions in US

Customary Units

2.7

Electrical Interfaces:

PL Processing

Launch Pad

Includes #pins, connector type, any accommodations for SV electrical e.g. SV battery charging while encapsulated

2.8 List of LV emitters and receivers

Power, frequency, Electromagnetic field [E-field] levels, and sensitivity of receivers

2.9

LV Radiated Emissions

Specific maximum radiated and conducted emissions levels that shall not be exceeded by the LV

2.10

Maximum (NTE) PL Radiated Emissions

Specific maximum radiated and conducted emissions levels that shall not be exceeded by the PL.

2.11

Separation

Separation system(s), commanding, detection, telemetry, inhibits, CCAM, separation state vector reporting

2.12 Payload Compartment Gas Conditioning

Standards and options provided for conditioned air and gaseous nitrogen

2.13 Temperature and Humidity

Standards and options provided for control and monitoring

2.14 Contamination Control

Standards and options for air quality, launch vehicle cleanliness, and CCAM

2.15

Flight Environments:

Dynamic Loads (Acceleration, Torsion)

Random and/or Sine Vibration

Acoustics

Shock

Fairing Depressurization

PL Temperature Exposure Free Molecular Heating (FMH)

LV capabilities and constraints for each flight environment

3 Services and Operations

3.1

LV Safety

Flight Termination System (FTS), orbital debris mitigation, C/CAM, safety documentation

3.2

Transportation Capabilities and Environments

Methods of transport, availability and type of environmental control system (ECS) and monitoring during transportation

3.3

Facilities

Includes security, classified processing certification, cranes, cleanroom, PPF, fueling

3.4

Mission Integration Services

Describes standard/optional services including: Coupled Loads Analysis (CLA), LV-SV Interface Control Document (ICD), etc.

3.5

Range Planning

Status of range planning with specific ranges, including infrastructure, range interface documents, FAA licensing, COLA, list of documents provided, document tailoring

3.6

Operations:

Ground Operations

Launch Operations

Flight Operations

Includes rollout through end of mission

3.7 Sample Mission Profile Sample event timeline for typical mission

3.8

Future Developments

Any developments in work that may be available in the future with projected availability date