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Contents

   



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1 Objectives  





2 Flight  





3 Gallery  





4 References  














Pad Abort Test 1: Difference between revisions






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{{distinguish|text=[[Pad Abort 1]], a 2010 Orion test flight}}

{{Infobox spaceflight<!--technically not a spaceflight, but template seems best fit for this article-->

{{Infobox spaceflight<!--technically not a spaceflight, but template seems best fit for this article-->

| name = Pad Abort Test 1

| name = Pad Abort Test 1


Revision as of 16:49, 23 May 2019

Pad Abort Test 1
Pad Abort Test 1 launch.
Mission typeAbort test
OperatorNASA
Mission duration2 minutes, 45.1 seconds
Distance travelled2.51 kilometers (1.56 mi)
Apogee2.82 kilometers (1.75 mi)
Spacecraft properties
SpacecraftApollo BP-06
Start of mission
Launch dateNovember 7, 1963, 16:00:01 (1963-11-07UTC16:00:01Z) UTC
RocketApollo LES
Launch siteWhite Sands LC-36
End of mission
Landing dateNovember 7, 1963, 16:02:45 (1963-11-07UTC16:02:46Z) UTC
Project Apollo
Abort tests
← QTV
A-001 →
 

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 able to pull the spacecraft away from an exploding rocket on the launch 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-06) 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

On November 7, 1963, an abort signal was sent to the LES at 09:00:01 local time. This began a sequence in which the main solid rockets fired to lift the spacecraft and smaller attitude rockets fired to move it laterally toward the ocean.

The LES separated after 15 seconds, allowing the spacecraft to take a ballistic trajectory. The parachute system worked perfectly: the drogue chute stabilized the spacecraft, then the three main parachutes slowed the descent to a leisurely 26 kilometers per hour.

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

Gallery

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

References


Retrieved from "https://en.wikipedia.org/w/index.php?title=Pad_Abort_Test_1&oldid=898447802"

Categories: 
Apollo program
1963 in spaceflight
Test spaceflights
Hidden categories: 
Commons category link is locally defined
Use American English from January 2014
All Wikipedia articles written in American English
 



This page was last edited on 23 May 2019, at 16:49 (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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