March 28, 2024

NASA’s Additional Artemis I Test Objectives for Space Launch System Rocket and Orion Spacecraft

Animation of the Orion spacecraft flying around the Moon. Credit: NASA.
During Artemis I, which is set up to launch as early as August 29, NASA plans to achieve several primary goals. These consist of demonstrating the efficiency of the Orion spacecrafts heat shield from lunar return velocities, demonstrating operations and facilities throughout all mission phases from launch countdown through recovery, and obtaining the crew module for post-flight analysis.
As the first incorporated flight of the Space Launch System rocket, Orion spacecraft, and the exploration ground systems at NASAs 21st century spaceport in Florida, engineers hope to achieve a host of additional test goals to much better comprehend how the spacecraft carries out in space and prepare for future objectives with crew.
Achieving additional goals helps decrease threat for objectives with a human crew aboard. This also offers extra data so engineers can evaluate patterns in spacecraft efficiency or improve self-confidence in spacecraft capabilities. A few of the extra goals prepared for the Artemis I objective include:

Modal study
On the European-built service module, Orion is equipped with 24 reaction control system (RCS) thrusters. These are little engines responsible for moving the spacecraft in different directions and turning it. The modal survey is a prescribed series of small RCS shootings that will help engineers ensure the structural margin of Orions solar selection wings throughout the mission. Flight controllers will command several small firings of the engines to cause the arrays to bend. They will measure the impact of the firings on the arrays and evaluate whether the inertial measurement units utilized for navigation are experiencing what they should. Till the modal survey is complete, big translational burns are limited to 40 seconds.
During Artemis I, the uncrewed Orion spacecraft will introduce on the most effective rocket in the world and travel countless miles beyond the Moon, farther than any spacecraft constructed for human beings has actually ever flown. Credit: NASA
Optical navigation electronic camera certification
This is responsible for constantly understanding where the spacecraft is situated in area, which way its pointed, and where its going. These sensitive cameras take photos of the star field around Orion, the Moon, and Earth, and compare the images to their built-in map of stars. The Optical navigation camera is a secondary electronic camera that takes images of the Moon and Earth to assist orient the spacecraft by looking at the size and position of the celestial bodies in the image.
Solar selection wing video camera Wi-Fi characterization
Electronic cameras attached to the pointers of the solar selection wings interact with Orions camera controller through an onboard Wi-Fi network. Flight controllers will differ the positioning of the solar selections to evaluate the Wi-Fi strength while the selections remain in various setups. The test will enable engineers to enhance how quickly imagery taken by electronic cameras on the ends of the selections can be transferred to onboard recorders.
Artemis I will be the very first incorporated flight test of NASAs deep space expedition system: the Orion spacecraft, Space Launch System (SLS) rocket and the ground systems at Kennedy Space Center in Cape Canaveral, Florida. Throughout this flight, the uncrewed Orion spacecraft will introduce on the most powerful rocket in the world and travel thousands of miles beyond the Moon, further than any spacecraft developed for people has actually ever flown, over the course of about a three-week mission.
Crew module/service module surveys
Flight controllers will use the cams on the 4 solar variety wings to take comprehensive images of the crew module and service module two times throughout the mission to identify any micrometeoroid or orbital debris strikes. A study performed early on in the objective will offer images not long after the spacecraft has flown beyond the elevation where area debris resides and a 2nd study on the return leg will take place several days before reentry.
Large file shipment protocol uplink
Engineers in mission control will uplink big information files to Orion to much better understand just how much time it considers the spacecraft to receive sizeable files. During the mission, flight controllers utilize the Deep Space Network to communicate with and send data to the spacecraft, but testing prior to the flight hasnt included utilizing the network. The test will assist notify engineers understanding of whether the spacecraft uplink and downlink capability suffices to support human score validation of end-to-end interaction prior to Artemis II, the first flight with astronauts.
Throughout Artemis I, Orion will venture countless miles beyond the moon during an approximately three-week objective. Credit: NASA
Star tracker thermal evaluation
Engineers want to define the alignment between the star trackers that belong to the control, navigation, and assistance system and the Orion inertial measurements units, by exposing various locations of the spacecraft to the Sun and triggering the star trackers in the different thermal states. The measurements will notify the unpredictability in the navigation state due to thermal bending and growth which eventually impacts the amount of propellant required for spacecraft maneuvers during crewed missions.
Radiator loop flow control
Two radiator loops on the spacecrafts European Service Module help expel heat created by different systems throughout the flight. Control mode allows for much better control of the radiator pumps and their flow rate, and will be utilized on crewed objectives when more refined control of flow through the radiators is wanted.
Artists impression of Orion over the Moon. Orion is NASAs next spacecraft to send humans into space. It is created to send astronauts further into space than ever before, beyond the Moon to asteroids and even Mars. The astronauts will enter our environment at speeds over 32,000 km/h however the capsule will protect them and guarantee a safe but bumpy landing when they return to Earth. Credit: NASA/ESA/ATG Medialab
Solar selection wing plume
Depending on the angle of Orions solar variety wings throughout some thruster shootings, the plume, or exhaust gasses, from those firings might increase the selections temperature. Through a series of small RCS shootings, engineers will gather information to define the heating of the solar variety wings.
Propellant slosh
Because of the lack of gravity in area, liquid propellant kept in tanks on the spacecraft moves differently in area than on Earth. Propellant movement, or slosh, in area is difficult to model on Earth, so engineers plan to collect information on the motion of the propellant during several planned activities during the objective.
Search acquire and track (SAT) mode
SAT mode is an algorithm meant to recuperate and preserve communications with Earth after loss of Orions navigation state, extended loss of communications with Earth, or after a momentary power loss that causes Orion to reboot hardware. To test the algorithm, flight controllers will command the spacecraft to enter SAT mode, and after about 15 minutes, restore typical communications. Testing SAT mode will give engineers confidence it can be trusted as the last choice to repair a loss of interactions when a team is aboard.
This artists rendering reveals a birds-eye view of the liftoff of NASAs Space Launch System (SLS) rocket. This Block 1 crew configuration of the rocket that will send out the very first 3 Artemis missions to the Moon. Credit: NASA/MSFC
Entry aerothermal
Throughout entry of the spacecraft through Earths environment, a recommended series of 19 reaction control system shootings on the crew module will be done to understand performance compared to predicted data for the sequence. Engineers are interested in gathering this information during high heating on the spacecraft where the aerothermal effects are largest.
Integrated Search and Rescue Satellite Aided Tracking (SARSAT) functionality
The SARSAT test will confirm connection in between beacons to be used by crew on future flights and ground stations getting the signal. The beacons will be remotely triggered and powered for about an hour after splashdown and will likewise help engineers comprehend whether the signal transmitted interferes with interactions devices used throughout recovery operations, including Orions built-in tri-band beacon which transmits the spacecrafts exact location after splashdown.
Ammonia boiler restart
After Artemis I splashdown, Orions ammonia boiler will be switched off for numerous minutes and then rebooted to provide additional information about the systems capability. Ammonia boilers are used to assist control the thermal aspects of the spacecraft to keep its power and avionics systems keep the interior and cool of the team module at a comfy temperature level for future teams. In some potential contingency landing circumstances for crewed objectives, teams may require to switch off the ammonia boiler to look for risks outside the spacecraft, then potentially turn it back on to supply additional cooling.
Engineers will carry out additional tests to gather data, including keeping an eye on the heatshield and interior parts for saltwater intrusion after splashdown. They likewise will check the GPS receiver on the spacecraft to figure out the spacecrafts ability to choose up the signal being sent around Earth, which might be utilized to augment the spacecrafts ability to comprehend its positioning in case of communications loss with objective controllers.
Jointly, performing extra goals throughout the flight provides extra info engineers can utilize to enhance Orion. This is vital as it is NASAs spacecraft that will take humans to deep area for several years to come.

Artemis I will be the very first integrated flight test of NASAs deep space expedition system: the Orion spacecraft, Space Launch System (SLS) rocket and the ground systems at Kennedy Space Center in Cape Canaveral, Florida. Throughout this flight, the uncrewed Orion spacecraft will introduce on the most powerful rocket in the world and travel thousands of miles beyond the Moon, further than any spacecraft developed for human beings has ever flown, over the course of about a three-week objective. Engineers in objective control will uplink big data files to Orion to better comprehend how much time it takes for the spacecraft to receive significant files. During the objective, flight controllers utilize the Deep Space Network to communicate with and send out information to the spacecraft, but screening prior to the flight hasnt consisted of using the network. Orion is NASAs next spacecraft to send humans into space.