N95- 19OO3 S 0 - NTRS - NASA

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module penetration. ... tip-to-tip distance with respect to the inner wall grain direction, and the ... Figure 1 shows the normal impact (i.e. 0=0) of a dual-wall.
N95- 19OO3 S 0 ;:J,,< .Q_ 1994 NASA/ASEE

SUMMER

FACULTY

MARSHALL SPACE THE UNIVERSITY

FELLOWSHIP

PROGRAM

FLIGHT CENTER OF ALABAMA

CRACKING CHARACTERISTICS OF A HABITABLE MODULE PRESSURE WALL FOLLOWING ORBITAL DEBRIS PENETRATION

Prepared

By:

William

P. Schonberg,

Academic

Rank:

Associate

Institution

and Department:

The University Department

Professor of Alabama

Laboratory: Division:

Structures Structural

Design

Branch:

Structural

Development

Colleague:

Dr. Joel Williamsen

XXXVI

in Huntsville

of Civil & Environmental

NASA/MSFC:

MSFC

Ph.D.

and Dynamics

Engineering

INTRODUCTION All long-duration meteoroids design

and pieces

consideration

presents

the results

magnitudes habitable predictions

cracking

penetration.

unzipping

unzipping

addition,

whose

occur

under lifetime

hole size predictions

creation analysis

for module

evacuation

of the phenomena

considered

include

prior to the onset

maximum

EXPERIMENTAL

Debris

spacecratt

Simulation

wall,

Facility

a blanket

[3].

of multi-layer

to determine

conditions.

in such an analysis. analysis

due to air loss.

maximum

tip-to-tip

AND

(MLI)

was

O

$2/S

crack

distance,

of thermal inserted

impacted by a at the NASA/MSFC insulation

between

in the

the bumper the lethality

and of the

Dp

BUMPER

v

AL 6061-T6 (_

ts

MLI BLANKET

T S

= 0.23,0.50,0.94

0.81 < ts < 2.03

Some

Lvo

11.12 mm

2.9 < Vp < 7.4 km/sec 0 < 0 < 75 deg 4.32 < S < 15.24 cm

to determine

DATA

the presence

mm

PRESSURE

WALL

AL 2219-T87_

_

tw

2.03 < t w < 4.83 mm twp=0.51

, 1.02 mm WITNESS

6061-T6

PLATES

_:::::_twp

AL Figure

1. Hypervelocity

Impact

EMPIRICAL

data;

Equations (1-19) Tables 1-3 provide

regression

equation

are the result corresponding

predictions,

of a Generic

PREDICTOR

Dual-Wall

standard

deviations

XxxvI-1

Structure

EQUATIONS

of a multiple linear regression average errors (in percent) of the errors

analysis between

performed on the actual data and

(also in percent),

of

In

of a survivability

inner wall. The witness plates behind the inner wall are used to characterize debris exiting the inner wall in the event of inner wall perforation.

4.75