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P1.26 AND THE U.S. MANNED PROGRAM: A BRIEF CHRONOLOGY

Steven B. Newman * Central Connecticut State University, New Britain, Connecticut

1. INTRODUCTION 2. PROJECT

The destruction of the shuttle Challenger The launch of Freedom 7(5/5/1961), with (STS-51) in January of 1986 illustrated the profound aboard, was the first U.S. manned space impact that weather can have on spaceflight operations. mission. As such, extreme care was exercised as to However, Challenger was just one of many manned weather conditions for launch. The mission was, in fact, space missions to be affected (in one way or another) scrubbed one day due to weather. On launch day, an by weather conditions either before, during, or after additional 20-45 minute weather delay was necessary. launch. This paper will provide a summary, beginning NASA (the National Aeronautics and Space with the earliest missions and Administration) maintained strict weather rules for continuing to the present day program, of launch throughout the Mercury program. Fig. 1 shows those operations that have been affected, for better or the weather typical of launch days for Project Mercury. worse, by meteorological conditions. Of the six manned Mercury , only one (Faith 7, aboard, 5/15/1963) was not scrubbed or delayed by weather prior to launch. In the case of Sigma 7 (Walter Schirra aboard, 10/2/1962), a hurricane near one of the recovery areas necessitated moving recovery ships some 215 miles downrange, but the launch proceeded as planned.

3.

By the time Project Gemini got under way in 1965, NASA had relaxed its launch rules slightly. Clear skies were no longer a requirement for launch. As such, only one of the 10 Gemini missions were scrubbed, (Gemini V), and that was more due to a computer problem than due to weather (there were thunderstorms near the ). In addition, the Gemini V Fig. 2. Gemini missions recovery was moved used a modified up one due to II Hurricane Betsy. While the Gemini IV launch was not affected by Fig. 1. into orbit atop an weather, there were concerns over Tropical Storms on 20 Babe and Carla near the recovery zones in the western Pacific. The aboard Gemini VIII, which was aborted early due to problems with the thrusters, landed outside the prime recovery zone, and * Corresponding author address: Steven B. Newman, the astronauts became seasick after waiting in high Physics & Sciences Department, Central seas for the recovery team to get to them. Connecticut State University, New Britain, CT 06050; e-mail: [email protected] later determined from photos and that the rocket had NOT, in fact, flown into a thunderstorm, but that the lightning was self-induced. Thus NASA was to say that Rule 1-404 had not been violated in this case. 12 was the first (and last) manned space to be launched into a rainstorm. , the aborted lunar landing mission had its recovery zone threatened by a tropical storm, but proceeded as planned.

Fig. 3. The launch of on 16 July 1969

4. APOLLO, and APOLLO-

The was remarkably free of weather related scrubs or delays. Only one launch () was delayed by weather, and there were no scrubs. The recovery zone for Apollo 11, the first lunar landing mission had to be moved due to weather, but the recovery itself was not affected.

4.1 The Near Tragedy of

There was one spectacular incident in November, 1969 that nearly cost the lives of the crew of Apollo 12. Fig. 4. Lightning strikes the launch tower just after During countdown, a cold front was observed moving the liftoff of Apollo 12, 14 November 1969 slowly southward across central . Skies were overcast at the Cape, and rainshowers were in the area. Not wanting to delay the flight, Mission Control decided 5. THE to waive Rule 1-404, which stated “The will not be launched when its NASA’s Space Transportation System (STS), more flight path will carry it through a commonly known as the space shuttle has been more a cumulonimbus (thunderstorm) cloud formation.” profoundly affected by weather than any of the previous The rule existed because the V rocket was not manned spaceflight projects. This became astoundingly designed to withstand thunderstorm conditions. Just 36 clear on the morning of 28 January 1986, when the seconds after launch, the spacecraft suffered a massive shuttle Challenger exploded just 74 seconds after lifting electrical anomaly. A second disturbance occurred just off into a clear, cold Florida morning. 16 seconds later. The guidance platform failed, as well Unusually cold weather at the as all other AC power in the spacecraft along with the in Florida had sent the temperature below freezing fuel cells. The crew reported their overnight, allowing icicles to form on the launchpad opinion that the rocket had been struck by lightning. It (Fig.5). The cold weather caused the rubber O-rings in was only through the quick thinking of ground controllers the solid rocket boosters (SRB) to lose their flexibility that the crew were able to restore their electrical power. and crack. During launch, the O-rings failed, allowing The mission continued without incident after that. It was flaming hot gasses to leak out of the side of one of the SRBs. The gasses penetrated the thin skin of the shuttle missions being forced to divert landing from the external fuel tank and caused a catastrophic in Florida to the dry lake bed at explosion, destroying the shuttle and killing the seven in California. crewmembers.

NASA Schedule of Weather Briefings Prior to Every Launch of the Space Shuttle L -2 4 hr 0 m in B riefing for F lig ht D irector and astronau ts L -2 1 hr 0 m in B riefing for rem ov al of R otating S erv ice S tru ctu re L -9 hr 0 0 m in B riefing for ex ternal tank fu el load ing L -4 hr 3 0 m in B riefing for S p ace S hu ttle L au nch D irector L -3 hr 5 5 m in B riefing for astronau ts L -2 hr 1 0 m in B riefing for F lig ht D irector L -0 hr 3 5 m in B riefing for lau nch and R T L S L -0 hr 1 3 m in Poll all weather constraints

6. REFERENCES

NASA Spaceflight Meteorology Group: Mercury Program Weather Support. http://www.srh.noaa.gov/smg/mercury.htm NASA Spaceflight Meteorology Group: Gemini Program Weather Support. http://www.srh.noaa.gov/smg/gemini.htm Fig. 5. Icicles on the launch pad of Challenger NASA Spaceflight Meteorology Support: Apollo (STS-51) on 28 January 1986 Program Weather Support. http://www.srh.noaa.gov/smg/apollo.htm Some engineers at Morton-, the company that Orloff, R.W., 2001: Apollo by the numbers. built the SRBs had argued against launching in such http://history.nasa.gov/SP-4029/SP-4029.htm cold weather, but were overruled by NASA Space Shuttle Weather administrators. Since that time, NASA has adhered to and KSC End of Mission Weather Landing Criteria a strict set of pre-launch rules that cannot be changed http://www.spaceref.com/news/viewpr.html?pid=686 or violated. Numerous weather briefings are held from 24 hours to just over 10 minutes prior to a space shuttle launch (see Table above right). In addition, there are strict rules for landing that have resulted in numerous

Su m m ary o f Weather-Related Im p acts o n Early U .S. M an n ed Sp ace Flig ht M issio n s Flig ht D ate Weather Related Effects F reed om 7 5 /5 /1 9 6 1 F irst m anned flig ht. O ne scru b . L au nch-d ay d elay d u e to low clou d s L ib erty B ell 7 7 /2 1 /1 9 6 1 S cru b b ed twice p lu s nu m erou s lau nch-d ay hold s F riend ship 7 2 /2 0 /1 9 6 2 F irst U .S . orb ital flig ht. S cru b b ed fou r tim es p rior to lau nch d ay A u rora 7 5 /2 4 /1 9 6 2 L au nch-d ay weather d elay s S ig m a 7 1 0 /3 /1 9 6 2 R ecov ery ship s m ov ed 2 0 0 + m iles d u e to threat of H u rricane D aisy G em ini V 8 /2 1 /1 9 6 5 O ne lau nch scru b . R ecov ery z one m ov ed d u e to H u rricane B etsy G em ini V III 3 /1 6 /1 9 6 6 R ecov ery in hig h seas led to astronau t m otion sick ness A p ollo 1 1 7 /1 6 /1 9 6 9 F irst lu nar land ing . R ecov ery z one m ov ed d u e to weather concerns A p ollo 1 2 1 1 /1 4 /1 9 6 9 S atu rn V stru ck twice b y lig htning after liftoff into a rainstorm A p ollo 1 3 4 /1 1 /1 9 7 0 R ecov ery z one threatened b y trop ical storm S T S -5 1 (C halleng er) 1 /2 8 /1 9 8 6 S u b -freez ing tem p eratu res led to O -ring failu re. V ehicle ex p lod ed . C rew of sev en lost