GSFC Experiment DUT Board for MPTB
INTRODUCTION
The Microelectronics and Photonics Testbed (MPTB) is a DoD-sponsored
effort being developed by the Naval Research Lab intended to sponsor
testing of microelectronics and photonics in a harsh radiation
environment. GSFC proposes to provide an experiment DUT board to
measure Bit Error Rate (BER) of emerging fiber optic data bus
transceivers as well as to measure single event upset (SEU) response
of devices previously flown on CRRES.
PRELIMINARY DESCRIPTION - fiber optic experiment
NASA/GSFC, jointly with the Naval Research Laboratory (NRL), has been
a leader in the development and/or implementation of fiber optic data
busses in spacecraft systems. The success of the MIL-STD-1773 fiber
optic data bus (or 1773 bus) on the Solar Anomalous Magnetospheric
Particle Explorer (SAMPEX) spacecraft, launched in July of 1992, has
paved the way towards the acceptance of fiber optics in the space
environment.
An extensive radiation ground test program was undertaken on the 1773
bus components prior to flight. This collaborative NASA/NRL effort led
to the formation of SEU models for fiber optic components as well as
accurate predictions of SAMPEX in-flight performance. Further ground
testing on other fiber optic components have extended these technology
and design-specific SEU models.
The 1773 bus, however, has its limitations. They include:
- Albeit the 1773 bus has a maximum signalling rate of 1 Mbps, its
actual effective data rate is limited to around 400 kbps. Thus, the
1773 bus is useful for low-speed applications such as the collection
of housekeeping telemetry on most spacecraft. And,
- The implementation of the 1773 bus on SAMPEX relies on SEU-sensitive
receiver design (both optically and electrically). Fortunately, a
combination of relatively low bus utilization (thus, allowing for
retransmission of unsuccessful messages) and protocol level error
handling exists and allows for a robust system. However, at higher
data rates and/or higher bus utilization rates, the system does not
have the luxury of retransmitting every message in error.
There is a potential solution: MIL-STD-1773A is a dual-rate (1 and 20
Mbps) fiber optic data bus that is emerging in many military, commercial,
and aerospace programs. The 20 Mbps data transfer rate covers the
requirements of >80% of spacecraft instruments. Additionally, two
separate transceiver designs exist (Boeing and Univ. of New Mexico NASA
Space Engineering Research Center), both of whose designs are hardened
to SEUs.
NASA/GSFC code 735.1, under NASA HQ/QW Research funding for emerging
technologies as well as potential funding from DNA, is preparing to
perform SEU ground tests on both transceiver designs before the end of
the calendar year.
We propose to develop an experiment for the MPTB program that will
perform in-flight BER measurements on both of the MIL-STD-1773A
transceivers as well as the current 1773 bus components. This experiment
provides validation of the fiber optic SEU models that have been
developed as well to provide further verification of the usability of
fiber optic systems in spaceflight applications.
PRELIMINARY DESCRIPTION - CRRES devices
Numerous spacecraft experience unexplained performance anomalies and
failures. It is suspected that many of these are due to the radiation
environment. In order to address this problem, it is desirable to obtain
reliable information from a controlled experiment about the impact of
the environment on known parts. For this purpose, it is proposed to
include the following part types on the NASA MPTB daughter board:
HS1-6504RH and AM-93L422. The use of these parts is considered
advantageous because extensive ground test data for TID and SEE is
available, and because these parts have in the past flown, and in some
cases, are still flying on several satellites (HST, TDRS, CRRES, etc...).
Thus, a controlled experiment with these devices provides a unique
opportunity to correlate the special data to be received from MPTB with
past and current spacecraft performance histories.