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Contents

   



(Top)
 


1 Objectives  





2 Flight  





3 External links  














Pad Abort Test 1






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From Wikipedia, the free encyclopedia
 


This is an old revision of this page, as edited by SunKing (talk | contribs)at06:37, 6 July 2006. The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.
(diff)  Previous revision | Latest revision (diff) | Newer revision  (diff)

Apollo Pad Abort Test 1
Apollo insignia
Mission statistics
Mission Name: Pad Abort Test 1
Call Sign: PA-1
Launch: November 7, 1963
16:00:01 UTC
White Sands Missile Range
Area 3
Landing: November 7, 1963
16:02:45 UTC
Duration: 2 min 45.1 s
Number of
Orbits:
Suborbital
Apogee: 1.75 mi (2.82 km)
Range: 1.56 mi (2.51 km)
PA-1

Pad Abort Test 1 was the first abort test of the Apollo spacecraft on November 7, 1963.

Objectives

Pad Abort Test 1 was a mission to investigate the effects on the Apollo spacecraft during an abort from the pad. The launch escape system (LES) had to be capable of pulling the spacecraft away from a possibly exploding rocket while it sat on the pad. The LES then had to gain enough altitude to allow the command module's parachutes to open, preferably with the spacecraft over water and not land.

The flight featured a production model LES and a boilerplate (BP-6) Apollo spacecraft, the first mission to feature one. The spacecraft carried no instruments for measuring structural loads as the capsule's boilerplate structure did not represent that of a real spacecraft.

Flight

Pad Abort Test 1 (NASA)

OnNovember 7, 1963, an abort signal was sent to the LES at 09:00:01 local time. This initiated a sequence where the main solid rockets fired to move the spacecraft craft and smaller attitude rockets fired so that the spacecraft moved laterally (atCape Canaveral this lateral movement would be towards the ocean).

The LES separated after fifteen seconds with the spacecraft now on a ballistic trajectory. The parachute system worked perfectly with the drogue chute stabilizing the spacecraft, followed by the three main parachutes that slowed the descent to a leisurely 26 kilometres per hour.

The only problems found with the flight were that the LES rockets had left a soot deposit on the spacecraft exterior and the stability of the spacecraft was less than predicted.

Apollo Pad Abort Test - Nov. 7, 1963 (NASA)

External links


Retrieved from "https://en.wikipedia.org/w/index.php?title=Pad_Abort_Test_1&oldid=62326008"

Categories: 
Apollo program
1963
 



This page was last edited on 6 July 2006, at 06:37 (UTC).

This version of the page has been revised. Besides normal editing, the reason for revision may have been that this version contains factual inaccuracies, vandalism, or material not compatible with the Creative Commons Attribution-ShareAlike License.



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