Decorative Menu Code

jump over navigation bar
NASA Orbital Debris Program Office
NASA Orbital Debris Program Office Navigation Bar
Navigation Bar Protection Shielding Collision Avoidance Navigation Bar
Home Page Home Page Contacts Home Page JSC Home Page NASA Home Page
jump over navigation bar
Home
NASA Orbital Debris Program Office
Modeling
Measurements
Protection
Mitigation
Remediation
Reentry
Quarterly New
NASA Links
Orbital Debris Shielding

Micro-Meteoroid Orbital Debris Shielding  

 


The Node 1, the first U.S. element to go up and attach with the Russian FGB (carried on STS-88), is protected by MMOD shields that protect the living area against micro meteoroid debris from penetrating the pressure hull.  Shown is the forward meteor debris shield C2-05 (jsc2007e097850).

Spacecraft shielding is designed to withstand a majority of the micrometeoroid and orbital debris (MMOD) particles that can impact a spacecraft, thus reducing the likelihood of serious damage to the vehicle and/or crew. Shielding is one part of an overall strategy to reduce impact risk that can also include collision warning and avoidance. Although it is not possible to eliminate all impact risk, shields are designed to meet or exceed probability-based protection limits.

 

 

Meteoroid and Orbital Debris Environment

 


Spacecraft shielding for Earth-orbiting satellites must protect against both the natural meteoroid and human made orbital debris which have very different velocity regimes. Orbital debris impact velocities in LEO have an average velocity of about 11 km/sec, concentrating an enormous amount of kinetic energy at the point of impact. Meteoroids have even higher velocities, averaging about 20 km/s and reaching velocities as high as 70 km/s.

 

Whipple Shield

 


Figure 1. (Top) Crater formed by a 6.4 mm aluminum sphere impacting at ~7 km/sec. The target is 3.7 cm thick aluminum. (Bottom) The same size and velocity impactor striking a simple Whipple shield with a front sheet thickness of 1.3 mm and a rear wall thickness of 3.2 mm separated by 10.2 cm. Both walls are made of the same aluminum material as the top thick wall.

One way to shield against MMOD impacts is to increase the thickness of the spacecraft wall so that the wall remains intact after the impact (see Figure 1). However, this significantly increases the weight of the spacecraft which must be launched into space. A smarter method is to use the “Whipple Shield” concept.

In the 1940s, Fred Whipple proposed a meteoroid shield for spacecraft, called the Whipple shield in recognition of his contribution. The Whipple shield consists of a thin, aluminum “sacrificial” wall mounted at a distance from a rear wall. The function of the first sheet or “BUMPER” is to break up the projectile into a cloud of material containing both projectile and BUMPER debris. This cloud expands while moving across the standoff, resulting in the impactor momentum being distributed over a wide area of the rear wall (Figure 2). The back sheet must be thick enough to withstand the blast loading from the debris cloud and any solid fragments that remain. For most conditions, a Whipple shield results in a significant weight reduction over a single plate, which must be strong enough to receive the projectile kinetic energy in a localized area.

Figure 2 (Top)

In recent years, improved shielding concepts have been developed to provide higher levels of spacecraft meteoroid and debris protection with less weight. The stuffed Whipple shield incorporates a blanket between the outer aluminum BUMPER and inner pressure wall that combines two materials: Nextel™ ceramic fabric and Kevlar™ high strength fabric. Other shielding concepts include a stuffed Whipple shield with a 30 cm standoff and a Nextel multi-shock shield. By using advanced shielding concepts, a reduction of up to 50% in mass can be achieved.

For more information on space craft shielding go here.

 

 

jump over navigation bar| Home | Modeling | Measurements | Protection | Mitigation | Reentry | Quarterly News |

 


NASA Web Accessibility, Privacy Policy and Important Notices
Responsible NASA Official: Eugene Stansbery
Web Curator: Mechelle Brown

  National Aeronautics Space Administration (NASA)
Johnson Space Center (JSC)
Last Updated: 02/03/2010