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A Loose Screw on HST: Its Effect on HST Observing Programs

A Loose Screw on HST: Its Effect on HST Observing Programs

J. Younger

July 22, 1999

Concurrence: G. Miller

Abstract

A hardware problem in the HST power system has caused overcharging of 2 of the 6 on-board batteries, which, if nothing was done, could result in battery overheating and possible failure. This, in combination with a general increase in power consumption by the newer on-board instruments, has led to a need to revise some spacecraft constraints in order to maintain adequate power to HST.

This report describes the actions taken by the NASA Goddard HST Project to address this need and their effect on the scheduling of HST observing programs

1. The Problem

In the spring of 1998 an anomaly showed up in the HST power system, indicating that a 20 milliohm resistance had developed in one of the power busses that combines power from batteries 5 and 6. An engineering analysis tentatively identified the fault as a loose screw connecting two copper bus bars. The net result of this fault is an imbalance in distribution of the load carried by all 6 batteries: batteries 5 and 6 carry less of the load during night time than the other batteries and therefore are discharged less rapidly.

This load imbalance causes two problems:

2. The Solution

One of the solar array segments has been removed from the circuit charging batteries 5 and 6. This reduces overcharging and avoids runaway situations, but the removal of a solar array segment reduces the overall power available to HST during daylight hours (only 17 of 20 array segments are now being used). In order for HST to remain power positive, the maximum sustained sun to solar array normal angle (sun incidence angle) has been reduced from 25 to 20 degrees. Also, in the past the arrays have been allowed to go up to a 35 degree sun incidence angle for brief periods of time (up to 4 orbits). Now this angle will be restricted to no more than 25 degrees for a single orbit.

The consequence of these new restrictions is to reduce the roll angle flexibility, the angle around the HST V1 axis or bore sight, used in scheduling the telescope. The magnitude of this effect is a function of the angle between the HST's V1 axis and the sun (the affected range is between 90 and 135 degrees) and can reduce the allowed roll flexibility by as much as 8.1 degrees (illustrated in the following table).

  1. Table 1. Old and new values of the maximum allowed off nominal roll
  2. V1/Sun angle

    (degrees)

    Old maximum off nominal roll allowed

    New maximum off nominal roll allowed

    93

    24.21

    16.74

    108

    25.46

    17.35

    132

    22.14

    21.76

3. Effect of the Changes on HST Observing Programs

This reduced flexibility in HST scheduling can affect programs having either restrictions in orientation or time (e.g., visits using special requirements such as ORIENT, ORIENT FROM, AFTER, BEFORE and BETWEEN).

 

Acknowledgements : The material in this report was adapted from a memo by Rodger Doxsey and discussions with Merle Reinhart, Dave Taylor, Glenn Miller, Bill Workman and Ian Jordan.