EP Overview.pdf

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Attached to
JSC Engineering, Technology and Science (JETS) II Federal contract opportunity
Solicitation number
80JSC021JETSII
Issued by
National Aeronautics and Space Administration Johnson Space Center

About this file

This document is a request for information notice for the JETS II engineering, technology and science services contract opportunity with the National Aeronautics and Space Administration Johnson Space Center. The RFI seeks capability statements from all interested parties, including small businesses and minority institutions, to determine the appropriate level of competition and small business subcontracting goals. Engineering design, development, sustaining engineering, analysis, assessment, technology development, test services, and laboratory operation and maintenance services are required for the Engineering and Science Directorates at JSC and other NASA centers. Responses are requested to include business information, customers and references, and must be submitted electronically to the point of contact by December 17, 2020. The Government reserves the right to set aside the contract for small, 8(a), women-owned, veteran-owned, economically disadvantaged women-owned small, or HUBZone businesses based on responses received. No solicitation currently exists and interested firms should monitor the beta.SAM.gov website for any future solicitation release.

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Text version

Propulsion & Power Division

EP Agenda

• Organization

• Core Domains

• Demographics

• Type of EP Work

• System Management

• GFE and Development Products

• Facilities

• Experts

• EP’s Future

EP Domains

- Loads and Structural DynamicsEX

- Project/Partner Lead Engineers

- System Engineers for Programs and Mid to High-Level Cross Discipline GFE

- Spacecraft Test & Verification

- Mid to High-Level Cross Discipline Project Management

- Process, Tools, and Standards Management

Propulsion Systems - Power Systems -

Fuel Cells/Electrolysis - Pyrotechnics -

Integrated ISRU - Hazardous Testing -

GN&C System/Software DDT&E - GN&C Flight Simulations -

Flight Mechanics, Trajectory & Mission Design -

Aero sciences Characterization - Aerodynamic Decelerators DDT&E -

- Environmental Control and Life Support (ECLSS)

Human Rated Software - Autonomy -

Robotics - Crew Exercise -

Simulation -

EA

Chief Engineers -

Active Thermal Control Extravehicular Activity (EVA) Includes Suits and Tools Flight Crew/Hab Systems Environmental Test

Human System Interfaces

(CHI)

Wireless and Communication Systems Command and Data Handling Radiation & EEE Parts

Structures, Fracture Control Thermal Design Materials and Processes Mechanical Design and Analysis

Develop Hardware

Integrate Systems

Test Subsystems

Support Missions

Advance Technology

GFE & In-line Riser Cutters ISRU Payloads Water Hammer A.

Battery/Chargers Pyro Devices Commercial GTA

L2&L3 SE&I

Agency Strategy

ISRU& Power Component ICD Subsystem perf.

System model verif.

Hazardous ESTA: Power/Batteries; Fluids/Propulsion/ISRU; Pyrotechnics

EP

DivisionSystem Management

O/S, IVV, CoFR, MER, Sustaining

Orion, Gateway

ISS, CCP, VV

STMD, HLS

Tech. Development Battery Safety Prop Transfer Ignition Reliability Low Shock Pyros

ISRU

Fuel Cell

EP Work – Covering the Entire lifecycle

EP Demographics Age Distribution

Education Level College Degrees

Electrical Engineering

Chemical Engineering Mechanical Engineering

Aerospace Engineering

Other

Other

Bachelor’s Degree

Master’s Degree Doctorate

Early Career < 7 Years

Mid- Career 7-25 Years

Late-Career > 25 Years

Total Civil Servants= 96 Total Contractors =91

System Management

Provide Expertise for Insight/Oversight of Human Spacecraft Power, Propulsion, and Pyrotechnic Systems

• ISS including all Visiting Vehicles

• Orion MPCV

• Commercial Crew

• Gateway including propellant transfer

• Human Landing System

Perform Targeted In-Line Tasks to Enable Better Insight/Oversight

• Passive Propagation Resistant battery development & test

• Propulsion water hammer analysis

• Pyrotechnic device development (cutters, frangible nuts)

• Pyroshock testing, both explosive and tunable beam

• OMS engine vibration testing

• Gateway Power Lab for multi-element integrated testing

CM - CM-SM Separation:

R&R Separation Bolt

Time Delay

DBA

CM - Side Hatch Release:

Pin Puller

Pin Pusher T-Handle

LPI

BTD

LAS:

S&A

TBI

SM - Spacecraft Separation:

SCSM Frangible Nut

DBA

CM – LRS, FBC, & LAS

Separations:

Thruster LAS-CM Frangible Nut

DBA

Drogue Mortar

Pilot Mortar FBC Mortar

Reefing Line Cutter Drogue Riser Cutter Main Riser CutterCM - CM Propulsion &

Uprighting:

Pyrovalve

NSI

ETLs and Manifolds distributed throughout system

SM - Fairing Separation:

Fairing Separation Bolt

Horizontal Frangible Joint Vertical Frangible Joint

DBA

SM - Umbilical Separation:

Umbilical Separation Bolt

Time Delay

DBA

Multiple Distributed Pyrotechnic Devices

In-Line Program Support

ORION

OMS Engine Vibration Testing

EP3

EP4

EP5 EP6

Mission & Anomaly Support

LREBA

Lithium-ion Rechargeable EVA Battery

LLB-2

Long Life Battery-2

LPGT

Lithium-ion Pistol Grip Tool Battery

SAFER

EVA Batteries

INTERNATIONAL

SPACE STATION

EP3

EP4

EP5 EP6

EP GFE Products

PYROTECHNICS (EP3)

NSI-3A

(GFE)

Riser Main Cutter

(GFE)

Frangible Nuts

(GFE)

Explosive Bolt

(GE)

BATTERIES & CHARGERS (EP5)

xEMU Battery

Lithium Long-Life Battery-2

Power Supply Assembly (xPSA) xEMU PLSS Battery Management System

EP Development Products

PROPULSION (EP4) ISRU/TEST (EP3/EP6)

SEEKER

Returns from

Cygnus

LOX Methane Igniter

In-Line Analysis

Thermal Vacuum / Lunar Dust Environment

Chamber

Light- WAVE Engineering Test

Unit

Screw Conveyor Dryer

Fuel Cell/TEST (EP3/EP6)

Regenerative Fuel Cell

HLS

Fuel Cell

Fuel Cell for Suborbital Flight

Solid Oxide Electrolyzer and

Fuel Cell

Production of O2 and Fuel from In-Situ Resources

EP Technology Products

ESTA Test Capability Technologies - battery, pyrotechnic, power generation, control & distribution, on-board propulsion (RCS, ACS), in-situ resource utilization (ISRU)

Gases - N2, He, Ar, O2, CH4, CO2, CO, H2 (not a complete list)

Liquids - LN2, LHe, LO2, LCH4, de-ionized water, IPA, oils (not a complete list)

Pressures - from 10-6 torr to 60,000 psi

Temperatures - from -453 °F to +2500 °F

ESTA conducts tests and operations in hazardous environments.

115 acres– North of JSC

ESTA Orientation Video

Now-2025: Robotic Precursor & Human Lunar Return

• Prospecting payload development & support (MOXIE, Lite WAVE)

• Robotic rover power system development (VIPER)

• ISRU technology development/demo (CaRD, Auger Dryer)

• Ignition Reliability risk reduction for LO2-H2/CH4

• Gateway on-orbit Propellant Transfer risk reduction

• Develop Lunar Dust TVAC Test capability

• Gateway Integrated Power test capability development

• Safe, high-performance batteries

• Fuel cell development & test (PEM-based)

• Low shock pyrotechnics

2026+: Sustained Lunar Presence & Mars Analogs

• Pilot-scale Lunar ISRU flight demonstration

• Human Rover power system development (LTV)

• Gateway Propellant Transfer and Lander Refueling

• Lunar Surface Power development & mobility integration

• Fully operational Lunar Dust TVAC Test capability

• ISRU derived additive manufacturing

Bright Future for EP Domains

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