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Annie Wargetz

OSIRIS-REx – Testing In Progress

Posted by Annie Wargetz

17-07-2015 15:12 CDT

Topics: mission status, asteroids, OSIRIS-REx, explaining technology

This article originally appeared at Dante Lauretta's blog and is reposted here with Annie Wargetz's permission. -Ed.

The OSIRIS-REx spacecraft is in the assembly and testing phase at Lockheed Martin’s facility outside of Denver, Colorado. The instruments have begun to arrive at the facility, with OTES and OVIRS being delivered in the past weeks.

While the OLA, OCAMS, and REXIS instruments continue working towards their deliveries, other hardware onsite at Lockheed is undergoing testing prior to installation. The hardware is put through tests here on Earth prior to launching into space.

One of the tests the hardware is put through is called vibration testing. Spacecraft are subject to high levels of vibrations during launch. The high level of noise emitted from rockets, the vibrations from the thrust of the rocket, and the atmospheric environment of launch all contribute to these vibrations the spacecraft experience during ascent.

Another series of tests includes placing the hardware into chambers that are sealed off and simulate the temperatures and pressures of space. These tests are referred to as the Thermal Vacuum tests, or TVAC tests.

Let’s take a look at some of the specific testing that the different pieces of hardware are undergoing.

The Sample Return Container

The Sample Return Container (SRC) is responsible for housing the sample once it is collected from Bennu and returning it to the surface of the Earth. Since the SRC will be re-entering Earth’s atmosphere after being released from the spacecraft itself, it must be balanced so that the re-entry trajectory is as straight as possible.

The SRC is spun at high speeds while being held in different orientations in order to test the balance of its mass.

SRC Open Spin Balance test

Lockheed Martin

SRC Open Spin Balance test
This is the SRC Open Spin Balance test. This test spins the SRC while it is in the open configuration. You can see the cylindrical structure on the left side which is where the sample head will be stored with the sample from Bennu.
SRC Horizontal Spin Test

Lockheed Martin

SRC Horizontal Spin Test
The SRC Horizontal Spin Test spins the SRC on its side and checks for the balancing of the SRC in this orientation.
Vertical SRC Spin Test

Lockheed Martin

Vertical SRC Spin Test
The Vertical SRC Spin Test checks that the SRC mass is balanced in this vertical orientation.

In addition to the spin tests, the SRC has also undergone vibration testing. The entire spacecraft experiences a high level of vibrations during the climb into space, so testing the individual components of the spacecraft allows for checking them out prior to launch.

OSIRIS-REx SRC vibration testing

Lockheed Martin

OSIRIS-REx SRC vibration testing
This picture shows the SRC attached to the fixture that will conduct the vibration testing.

The SRC also has gone through thermal vacuum, or TVAC, testing which exposes the hardware to the extreme temperatures and low pressures of space.

OSIRIS-REx SRC in TVAC chamber

Lockheed Martin

OSIRIS-REx SRC in TVAC chamber
The SRC in the TVAC chamber prior to testing.

The TAGSAM Sampling Mechanism

These pictures show the progress being made on the TAGSAM instrument which will be responsible for executing the sampling sequence. The arm will extend from the spacecraft, placing the sample head on the surface of Bennu so that the sample can be collected.

OSIRIS-REx TAGSAM sample head

Lockheed Martin

OSIRIS-REx TAGSAM sample head
The sample head at the end of the TAGSAM mechanism is being inserted into the fixture it will reside in during the vibration testing.

Once the TAGSAM instrument is mounted to the vibration testing apparatus, the vibration testing is conducted.

OSIRIS-REx TAGSAM arm and sample container

Lockheed Martin

OSIRIS-REx TAGSAM arm and sample container
The TAGSAM arm and sample container (inside the dark grey enclosure) undergoing vibration testing.

In addition to the vibration testing, the TAGSAM instrument has been undergoing functional testing. Large balloons filled with helium are affixed to the instrument to offset the effects of gravity on the instrument. TAGSAM is then moved to test its range of motion.

OSIRIS-REx TAGSAM functional testing

Lockheed Martin

OSIRIS-REx TAGSAM functional testing
The TAGSAM instrument undergoing functional testing which tested its movement while a helium balloon was attached to it to simulate a microgravity environment.

The High Gain Antenna

The High Gain Antenna (HGA) is the most powerful communications antenna on the spacecraft. It will play a fundamental role in communicating with Earth during the mission via NASA’s Deep Space Network. It is also undergoing testing in preparation for installation onto the main spacecraft structure.

OSIRIS-REx HGA fit check

Lockheed Martin

OSIRIS-REx HGA fit check
Here, the HGA undergoes a fit check. The main spacecraft structure is behind the HGA and the clean room engineers are checking the alignment where the HGA will be installed onto the spacecraft.
OSIRIS-REx High Gain Antenna

Lockheed Martin

OSIRIS-REx High Gain Antenna
This image of the HGA shows what it looks like up close. You can see the truss support for the reflector and the high gain X-band golden cone coming out of the center of the main black reflector dish.
See other posts from July 2015


Or read more blog entries about: mission status, asteroids, OSIRIS-REx, explaining technology


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