ACES |
Advanced Cryogenic Evolved Stage, the ULA new Upper Stage for Vulcan rocket |
AE |
Ascent Element (HLS terminology) |
ANSMET |
Antarctic Search for Meteorites (NSF funded program in USA) |
ARES |
Astromaterials Research and Exploration Science Division at NASA JSC |
ATV |
All-Terrain Vehicle (FLARE terminology) or Automated Transfer Vehicle (basis of ESM) |
CC |
Crew Capsule (HLS terminology) |
CFM |
Cryogenic Fluid Management (HLS terminology) |
CIII |
Centaur III upper-stage built by ULA for Atlas V rocket |
CLV |
Commercial Launch Vehicle delivering payload to LEO or TLI (HLS terminology) |
CM |
Apollo Command Module |
COPV |
Composite Overwrap Pressure Vessels, component of the FLARE AE |
CV |
Centaur V upper-stage built by ULA for Vulcan rocket |
DAC |
Design Assessment Cycle, NASA evaluation of architectures for Artemis program |
DAE |
Fused (single-stage) Descent-Ascent Element, Combined (HLS terminology) |
DE |
Descent Element (HLS terminology) |
DoD |
Department of Defense |
ECPO |
Elliptical Coplanar Posigrade Orbit, a possible orbit being studied by HLS for Artemis |
EML1 |
Earth-Moon L1 point |
EML2 |
Earth-Moon L2 point |
EOR |
Earth Orbit Rendezvous, a concept considered for Apollo stages before TLI |
ESA |
European Space Agency |
ESM |
European Service Module (based on Automated Transfer Vehicle, ATV) |
F9 |
Falcon 9 built by SpaceX |
FH |
Falcon Heavy built by SpaceX |
FLARE |
Flexible Lunar Architecture for Exploration, an alternate architecture scenario for NASA's Artemis Program |
HALO |
Habitation and Logistics Outpost (former "Mini-Hab" Gateway component before 2019) |
HEO |
High Earth Orbit |
HLS |
Human Landing System (HLS) - NASA team developing the Artemis human lander |
ICPS |
Interim Cryogenic Propulsion Stage (ICPS), upper-stage for the NASA SLS Block 1 |
ISS |
International Space Station, NASA vehicle located in Earth's LLO at 51.6° inclination |
LLFPO |
Low Lunar Frozen Polar Orbit, a specific LLO at 86.5° inclination |
LBM |
Lunar Braking Module, a concept not adopted by Apollo using EOR |
LEM |
Lunar Excursion Module (LEM), later Lunar Module (LM) from the NASA Apollo program |
LEO |
Low Earth Orbit, for FLARE defined as a 28.5° inclination, 400 km circular Earth orbit |
LES |
Orion Launch and Entry Suit |
LLO |
Low Lunar Orbit, for FLARE a 100 km circular orbit above the lunar surface |
LOI |
Low Orbit Insertion burn to place a vehicle in orbit around the Moon |
LORAD |
Lunar Operations with Reuse and Assisted Descent (HLS terminology) |
LATV |
Lunar All-Terrain Vehicle (FLARE terminology) for a 1-person, 3-wheel electric vehicle |
LTV |
Lunar Terrain Vehicle, 4-wheel, 2-person “buggy” style lunar rover |
MH |
Minihab module (derived from the Cygnus vehicle) component of the Gateway vehicle |
MMH |
Mono-Methyl Hydrazine, CH3(NH)NH2, storable rocket propellant |
MMOD |
Micro-Meteoroid and Orbital Debris |
MPCV |
Multi-Purpose Crew Vehicle, another name for NASA's Orion capsule |
MPS |
Main Propulsion System (HLS terminology) |
NextSTEP |
Next Space Technologies for Exploration Partnerships: NASA public-private partnership |
NRHO |
Near Rectilinear Halo Orbit (rp = 3300 km, ra = 65,000 km in HLS terminology) |
NSF |
National Science Foundation |
OCSS |
Orion Crew Survival System (OCSS), orange colored ascent/entry suits for NASA crew |
OME |
Orbital Maneuvering Engine, part of the ESM and lunar lander AE |
PF |
Performance Fraction, a method to estimate delivery of mass to certain ΔV targets |
PIR |
Persistently Illuminated Regions of the Moon (near the poles) |
PMF |
Propellant Mass Fraction (HLS terminology) |
PPE |
Power and Propulsion Element, component of the Gateway vehicle |
PSR |
Permanently Shadowed Region on the Moon (near poles) |
RCS |
Reaction Control System |
RF |
Radio Frequency |
RFID |
Radio Frequency Identification |
RMS |
Remote Manipulator System, a mechanical arm for spacecraft to move external objects |
RPOD |
Rendezvous, Proximity Operations and Docking phases of mating vehicles in orbit |
RST |
Return SpaceTug (FLARE terminology), vehicle pushing Orion + ESM to Earth from Moon |
SLS |
Space Launch System, a proposed family of rockets being developed by NASA |
SLS B1 |
SLS Block 1 rocket, which delivers up to 26 mt to TLI (HLS terminology) |
SM |
Apollo Service Module |
TA |
Tug Adaptor (FLARE terminology), equipment to convert a Centaur US into a SpaceTug |
TCM |
Trajectory Correction Maneuver |
TE |
Transfer Element (HLS terminology) |
TE1 |
TE for AE/DAE for orbit to orbit transfer or initial braking (HLS terminology) |
TE2 |
TE for TE1 and provides orbit to orbit transfer and/or initial deorbit (HLS terminology) |
TEI |
Trans-Earth Injection burn to send a vehicle into the Earth's gravity field |
TLI |
Trans-Lunar Injection burn to send a vehicle into the Moon's gravity field |
TRL |
Technology Readiness Level |
ULA |
United Launch Alliance, rocket company formed in 2006 |
USA |
United States of America |
xEMU |
Exploration Extravehicular Mobility Unit, NASA space suit for lunar surface exploration |
ZBO |
Zero Boil-Off, concepts to limit the loss of cryogenic LOX/LH2 in spacecraft |