The document discusses NASA's plans for future human space exploration missions. It describes:
1) The upcoming year-long mission to the International Space Station by astronaut Scott Kelly and cosmonaut Mikhail Kornienko in 2015, which will be the longest mission ever by a US astronaut. Studies on this mission include the effects of long-term spaceflight on the human body.
2) Development of the Space Launch System, Orion spacecraft, and ground systems to enable human exploration beyond low Earth orbit to destinations like Mars.
3) Plans to use cis-lunar space and a distant retrograde orbit around the Moon as a "Proving Ground" to test technologies and operations required for human
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Goddard 2015: Greg Williams, NASA
1. National Aeronautics and Space Administration
Goddard Memorial
Symposium
Greg Williams
Deputy Associate Administrator
for Human Exploration and Operations
6. 6
ISS One-Year Mission
6
• 2015 marks the launch of astronaut Scott
Kelly and cosmonaut Mikhail Kornienko to
the ISS for 12 months – the longest mission
ever assigned to a US astronaut
– Joint US/Russian ISS research includes
studies on: ocular health, immune and
cardiovascular systems, cognitive
performance testing, and effectiveness of
countermeasure against bone and muscle
loss
• HRP study of identical twins astronaut
Scott Kelly, and retired astronaut, Mark
Kelly
– Provides unprecedented opportunity to
research effects of spaceflight on twin
genetic makeup, and better understand the
impacts of spaceflight on the human body
Retired astronaut Mark Kelly
(left) and his twin brother,
astronaut Scott Kelly, who will
spend a year on ISS
Scott Kelly
STS-103, STS-118, ISS 25/26
Mikhail Kornienko ISS 23/24
http://www.nasa.gov/exploration/humanresearch/index.html
8. Beginning human exploration
beyond LEO as soon as
practicable helps secure
our future in space.
Orion
Crew Capsule
Space
Launch
System
Ground Systems
Development & Operations
SLS, Orion, and Ground Systems
8
9. Ogive panels installed, Orion moved to launch pad Orion / Delta ready on pad ready for launch Service Module Panel Jettison
Parachutes deploy after EFT-1 flight EM-1 Pathfinder Barrel machining EM-1 Tunnel Machining
Orion Accomplishments
9
10. Booster installed at ATK for
Qualification Motor-1 test in March
RS-25 testing for SLS begins at
Stennis Space Center
Delivery of new engine controller unit
for RS-25 engines
SLS Stage Adapter flies successfully on
Orion’s EFT-1 launch
Construction begins on core stage test stands at
Marshall Space Flight Center
First flight barrel section produced at
Michoud Assembly Facility
SLS Accomplishments
10
10
11. GSDO Accomplishments
Anchorage.
The Orion crew module recovered Dec. 5 after
splashdown In the Pacific Ocean
Upgrades and modifications continue
on the 175-ton crane inside the VAB
- Modifications continue on the Mobile Launcher at
Kennedy Space Center Florida. 11
11
12. 12
VALIDATE
• Advanced Solar Electric Propulsion (SEP) systems to move large
masses in interplanetary space
• LDRO as a staging point for large cargo masses en route to Mars
• SLS and Orion in deep space
• Long duration, deep space habitation systems
• Crew health and performance in a deep space environment
• In-Situ Resource Utilization in micro-g
• Operations with reduced logistics capability
• Structures and mechanisms
CONDUCT
• EVAs in deep space with sample handling in micro-g
• Integrated human and robotic mission operations
• Capability Pathfinder and SKG missions
Enabling Human Missions to Mars
PROVING GROUND OBJECTIVES
13. 13
Cis-Lunar Space:
How the Earth and the Moon Interact
The contours on the plot depict energy states in the Earth-Moon
System and the relative difficulty of moving from one place to another.
A spacecraft at L2 is actually orbiting Earth
at a distance just past the Moon, however
if you look at it from the Moon, the orbit will
look like an ellipse around a point in space
giving them the name “halo orbits”.
The interaction of the Earth and Moon creates
bends in the energy contours that can be used
to lower the energy needed to move around
the Earth-Moon system and beyond, such as
this example of a low energy transfer between
L1 and L2 .
The Lunar Distant Retrograde Orbit leverages these
equilibrium and low energy contours to enable a stable
orbit with respect to the Earth and Moon, that is
accessible with about the same energy as L1 or L2.
Family of DROs in Earth-Moon Plane
14. ARM is a Stepping Stone to Higher Power SEP
Needed to Support Human Missions to Mars
1 10 100 1000
Solar Array Power (kW)
Deep Space 1 Dawn ARM
SEP
Mars Cargo
Chem/SEP
Mars Crew
1 10 100 1000
Solar Array Power (kW)
Deep Space 1 Dawn
SEP
Mars Cargo
Chem/SEP
Mars Crew
Asteroid Redirect
50 kW 50-100 kW 100-700 kW 300-700 kW
ARM Cis-Lunar Mission Mars Moons Mars Surface
14
15. Split Mission Concept
15
15
Using SEP for pre-emplacement of cargo and destination systems enables
sustainable Mars campaign
• Minimizes the cargo needed to be transported with the crew on future launches
• Enables a more sustainable launch cadence
• Pre-positions assets for crew missions, allowing for system checkout in the Mars
vicinity prior to committing to crew portion of mission
16. Split Mission Concept
16
DRO as an aggregation point for Mars habitation systems
• Provides a stable environment and ease of access for testing Proving Ground
capabilities
• Allows for Mars transit vehicle build-up and checkout in the deep-space environment
prior to crew departure
• Able to transfer Mars Transit Vehicle from DRO to High Earth Orbit with small amount
of propellant to rendezvous with crew in Orion – HEO is more efficient location to
leave Earth-moon system for Mars vicinity 16
17. Split Mission Concept
• Returning from Mars, the crew will return to Earth in Orion and
the Mars Transit Habitat will return to the staging point in cis-
lunar space for refurbishment in support of future missions 17
18. View From The Surface of Phobos
18
Expand human presence into
the solar system and to the
surface of Mars to advance
exploration, science,
innovation, benefits to
humanity, and international
collaboration.
Hinweis der Redaktion
In a few months, NASA will send an ocean wind-monitoring instrument to a berth on the International Space Station. That unique vantage point will give ISS-RapidScat, short for the International Space Station Rapid Scatterometer, the ability to observe daily (also called diurnal) cycles of wind created by solar heat.
1. The two-minute, full-duration static test -- scheduled for March 11 at booster prime contractor ATK's test facility in Promontory, Utah -- is a huge milestone for the program and will qualify the booster design for high temperature conditions. Once this test and a second, low-temperature test planned for early 2016 are complete, the hardware is qualified and ready for the first flight of SLS.
2. The RS-25, formerly the space shuttle main engine, fired up for 500 seconds on the A-1 test stand at Stennis, providing NASA engineers critical data on the engine controller unit and inlet pressure conditions. This is the first hot fire of an RS-25 engine since the end of space shuttle main engine testing in 2009. Four RS-25 engines will power SLS on future missions, including to an asteroid and Mars.
3. The new Engine Controller Unit allows communication between the vehicle and the engine, relaying commands to the engine and transmitting data back to the vehicle. It also provides closed-loop management of the engine by regulating the thrust and fuel mixture ratio while monitoring the engine's health and status. Controller development is based heavily on the recent development experience with the J-2X engine controller.
4. For Exploration Flight Test-1, Orion was mated to the Delta 4 Heavy launch vehicle with the Multipurpose Crew Vehicle-to-Stage Adapter, designed for commonality between EFT-1 and Orion’s first launch on SLS on Exploration Mission-1. The MSA performed nominally during the EFT-1 launch.
5. The barrel for the engine section of NASA's new rocket, the Space Launch System, is taken off the Vertical Weld Center at NASA's Michoud Assembly Facility in New Orleans. The barrel is flight hardware to be used on the first uncrewed test flight of the 70-metric-ton configuration of the rocket. The engine section, made up of the barrel and a ring -- also welded at Michoud -- will hold four RS-25 engines that will power the core stage of the SLS
6. A new, 215-foot test stand at NASA's Marshall Space Flight Center in Huntsville, Alabama, Test Stand 4693 will be used for structural loads testing on the liquid hydrogen tank for the core stage of NASA's Space Launch System. The core stage, towering more than 200 feet tall, will store cryogenic liquid hydrogen and liquid oxygen that will feed the vehicle’s RS-25 engines. SLS will be the most powerful rocket ever built for deep space missions, including to an asteroid and ultimately Mars.
The 4693 structure -- being built on the foundation of the stand where the Saturn V F-1 engine was tested -- will have a twin-tower configuration and be made with 2,150 tons of steel. The liquid hydrogen tank will be placed in the stand vertically, and be loaded with liquid nitrogen for stress testing. A second test stand also is under construction at the Marshall Center and will be used to test the liquid oxygen tank. The stands are on track to being completed in 2015.
Top left: Recovery Operations - The Orion crew module was recovered Dec. 5 after splashdown in the Pacific Ocean about 600 miles off the coast of San Diego, California. NASA, the U.S. Navy and Lockheed Martin coordinated efforts to recover Orion and secure the spacecraft inside the well deck of the USS Anchorage.
Bottom: VAB - Upgrades and modifications continue on the 175-ton crane inside the Vehicle Assembly Building at NASA's Kennedy Space Center in Florida. The crane's 45-year-old controls are being upgraded to improve reliability, precision and safety. The Ground Systems Development and Operations Program is overseeing upgrades and modifications to the crane so that it can support lifting needs for NASA and other exploration vehicles, including the agency's Space Launch System and Orion spacecraft.
Right: ML - Modifications continue on the Mobile Launcher at the Mobile Launcher Park Site at NASA’s Kennedy Space Center in Florida. A crane is being used to move scaffolding, or work platforms, around the base of the tower on the ML to continue upgrades and modifications to the structure. The ML is being modified and strengthened to accommodate the weight, size and thrust at launch of NASA's Space Launch System, or SLS, and Orion spacecraft. The ML is one of the key elements of ground support equipment that is being upgraded by the Ground Systems Development and Operations Program at Kennedy.