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4 min read<\/p>\n
As chief of test operations at NASA\u2019s Stennis Space Center, Maury Vander has been involved in some long-duration propulsion hot fires \u2013 but he still struggles to describe a pair of 34-minute space shuttle main engine tests conducted onsite in August 1988.<\/p>\n
\u201cWhen you stop and think about it, \u2026\u201d Vander begins, then pauses. \u201cIn 34 minutes, I can leave work and drive home to Slidell (15-20 miles west in Louisiana) and be relaxing in my recliner in that amount of time.\u201d<\/p>\n
Vander\u2019s struggle is understandable when one considers the numbers. On Aug. 3 and Aug. 15, operators at the Thad Cochran Test Stand (B-1) at NASA Stennis near Bay St. Louis, Mississippi, fired a space shuttle main engine for a total of 2,017 seconds each day, more than four times as long as the engine fired (500 seconds) during a typical space shuttle launch.<\/p>\n
In terms of propulsion firings, nothing else comes close. The next-longest duration appears to have occurred in 2001, when a Progress M1-5 engine was fired for about 22 minutes to help deorbit the Russian space station Mir.<\/p>\n
Vander still wonders at the south Mississippi feat. \u201cThe ability to juggle the type of challenges seen over the course of 30-plus minutes is amazing,\u201d he said. \u201cAnd you are not talking about 21st<\/sup> century technology either. You are talking about rather simplistic stuff not far removed from the 1960s, so there was an art to operating that type of equipment. But, they pulled it off.\u201d<\/p>\n NASA Stennis may have been the only place such a firing could have been conducted.<\/p>\n It had the needed test facility. The Thad Cochran (B-1) stand featured a larger liquid oxygen tank to support the test and was equipped with a diffuser that allowed operators to throttle the engine to lower power levels, thus conserving fuel. The stand also had a larger dock area for additional propellant barges needed for test support.<\/p>\n Each 34-minute test required about 600,000 gallons of liquid hydrogen and 230,000 gallons of liquid oxygen. Careful coordination ensured proper propellant flow from barges. \u201cWe still had old pumps for the barges, as opposed to the new ones that have variable drives to help control flow,\u201d Vander noted. \u201cThe pumps back then were basically on\/off pumps. If they were running, they were pretty much running wide open. That posed a challenge for controlling flow. It was a real art to orchestrate everything for such a long period of time.\u201d<\/p>\n In addition, the NASA Stennis High Pressure Gas Facility had to ensure proper volume and flow of gases to support the tests. Teams at the High Pressure Water Facility had to manage uninterrupted flow from the 66-million gallon reservoir to the test stand. \u201cAll of these were challenges they had to think their way through and logistically make happen,\u201d Vander said.<\/p>\n The test team had to maintain constant vigilance of such operations. \u201cYou are always monitoring, trying to figure out what could go wrong,\u201d Vander said. \u201cAt any given moment, you may have to react and deal with a problem. To think of those people sitting in front of computer screens, gauges, and such, watching and making sure their responsibilities were covered for 30-plus minutes, is just amazing.\u201d<\/p>\n The teams were driven by a compelling factor. The nation was just recovering from the Challenger tragedy of 1986. Space shuttle Discovery would launch NASA\u2019s return to flight in late September. Space shuttle Atlantis was scheduled to launch later in the year, but there was an issue with the fuel preburner injector on one of the engines. To resolve the matter, operators needed to record 8,000 seconds of hot fire on the injector. They decided to compile the time as efficiently as possible.<\/p>\n