Have there been any spacecraft with internal SRM other than CONTOUR?

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I read about the CONTOUR mission which used an internal solid rocket motor to change the trajectory. Have there been other spacecraft using a solid rocket motor which is not jettisoned after usage?










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    I read about the CONTOUR mission which used an internal solid rocket motor to change the trajectory. Have there been other spacecraft using a solid rocket motor which is not jettisoned after usage?










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      I read about the CONTOUR mission which used an internal solid rocket motor to change the trajectory. Have there been other spacecraft using a solid rocket motor which is not jettisoned after usage?










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      I read about the CONTOUR mission which used an internal solid rocket motor to change the trajectory. Have there been other spacecraft using a solid rocket motor which is not jettisoned after usage?







      spacecraft mission-design solid-fuel






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          2 Answers
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          The Soyuz descent module has SRMs that are fired just before touchdown. Does that count?






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            Muses A Lunar Orbiter (Hagoromo)



            above: from Gunter's Space Page




            According to Gunter's Space Page's Muses A Lunar Orbiter (Hagoromo):




            It was launched piggy-back on the Muses A (Hiten) probe into a highly elliptical Earth orbit which passed by the Moon ten times during the mission. At 19:37 UT on 18 March 1990 as Hiten approached its first lunar flyby, the small Hagoromo spacecraft was released into lunar orbit, making Japan the third nation to orbit the Moon. Although the S-band transmitter aboard Hagoromo had failed on 21 February 1990, the ignition of the Hagoromo deceleration rocket was confirmed by ground observation at 20:04:03 UT, the estimated orbit was 7400 × 20000 km with a period of 2.01 days. No contact could be established after orbit insertion.




            @DavidHammen's answer to the question "Was Hagoromo's capture into lunar orbit ballistic capture or more propulsive?":




            From the NASA Space Science Data Coordinated Archive entry on Hagoromo,




            A solid propellant (KM-L) retrorocket with a mass of 4 kg was mounted inside the spacecraft for orbit insertion.





            @DavidHammen's answer to the question "How could tiny Hagoromo have been seen visually from earth confirming its lunar orbit?" is a click away and worth the read, so I won't re-quote it here.



            See both (either) linked question for more images of this kawaii spacecraft and it's "parent" craft.






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              2 Answers
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              up vote
              2
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              The Soyuz descent module has SRMs that are fired just before touchdown. Does that count?






              share|improve this answer
























                up vote
                2
                down vote













                The Soyuz descent module has SRMs that are fired just before touchdown. Does that count?






                share|improve this answer






















                  up vote
                  2
                  down vote










                  up vote
                  2
                  down vote









                  The Soyuz descent module has SRMs that are fired just before touchdown. Does that count?






                  share|improve this answer












                  The Soyuz descent module has SRMs that are fired just before touchdown. Does that count?







                  share|improve this answer












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                  answered 2 hours ago









                  Hobbes

                  76.3k2210350




                  76.3k2210350




















                      up vote
                      1
                      down vote













                      Muses A Lunar Orbiter (Hagoromo)



                      above: from Gunter's Space Page




                      According to Gunter's Space Page's Muses A Lunar Orbiter (Hagoromo):




                      It was launched piggy-back on the Muses A (Hiten) probe into a highly elliptical Earth orbit which passed by the Moon ten times during the mission. At 19:37 UT on 18 March 1990 as Hiten approached its first lunar flyby, the small Hagoromo spacecraft was released into lunar orbit, making Japan the third nation to orbit the Moon. Although the S-band transmitter aboard Hagoromo had failed on 21 February 1990, the ignition of the Hagoromo deceleration rocket was confirmed by ground observation at 20:04:03 UT, the estimated orbit was 7400 × 20000 km with a period of 2.01 days. No contact could be established after orbit insertion.




                      @DavidHammen's answer to the question "Was Hagoromo's capture into lunar orbit ballistic capture or more propulsive?":




                      From the NASA Space Science Data Coordinated Archive entry on Hagoromo,




                      A solid propellant (KM-L) retrorocket with a mass of 4 kg was mounted inside the spacecraft for orbit insertion.





                      @DavidHammen's answer to the question "How could tiny Hagoromo have been seen visually from earth confirming its lunar orbit?" is a click away and worth the read, so I won't re-quote it here.



                      See both (either) linked question for more images of this kawaii spacecraft and it's "parent" craft.






                      share|improve this answer


























                        up vote
                        1
                        down vote













                        Muses A Lunar Orbiter (Hagoromo)



                        above: from Gunter's Space Page




                        According to Gunter's Space Page's Muses A Lunar Orbiter (Hagoromo):




                        It was launched piggy-back on the Muses A (Hiten) probe into a highly elliptical Earth orbit which passed by the Moon ten times during the mission. At 19:37 UT on 18 March 1990 as Hiten approached its first lunar flyby, the small Hagoromo spacecraft was released into lunar orbit, making Japan the third nation to orbit the Moon. Although the S-band transmitter aboard Hagoromo had failed on 21 February 1990, the ignition of the Hagoromo deceleration rocket was confirmed by ground observation at 20:04:03 UT, the estimated orbit was 7400 × 20000 km with a period of 2.01 days. No contact could be established after orbit insertion.




                        @DavidHammen's answer to the question "Was Hagoromo's capture into lunar orbit ballistic capture or more propulsive?":




                        From the NASA Space Science Data Coordinated Archive entry on Hagoromo,




                        A solid propellant (KM-L) retrorocket with a mass of 4 kg was mounted inside the spacecraft for orbit insertion.





                        @DavidHammen's answer to the question "How could tiny Hagoromo have been seen visually from earth confirming its lunar orbit?" is a click away and worth the read, so I won't re-quote it here.



                        See both (either) linked question for more images of this kawaii spacecraft and it's "parent" craft.






                        share|improve this answer
























                          up vote
                          1
                          down vote










                          up vote
                          1
                          down vote









                          Muses A Lunar Orbiter (Hagoromo)



                          above: from Gunter's Space Page




                          According to Gunter's Space Page's Muses A Lunar Orbiter (Hagoromo):




                          It was launched piggy-back on the Muses A (Hiten) probe into a highly elliptical Earth orbit which passed by the Moon ten times during the mission. At 19:37 UT on 18 March 1990 as Hiten approached its first lunar flyby, the small Hagoromo spacecraft was released into lunar orbit, making Japan the third nation to orbit the Moon. Although the S-band transmitter aboard Hagoromo had failed on 21 February 1990, the ignition of the Hagoromo deceleration rocket was confirmed by ground observation at 20:04:03 UT, the estimated orbit was 7400 × 20000 km with a period of 2.01 days. No contact could be established after orbit insertion.




                          @DavidHammen's answer to the question "Was Hagoromo's capture into lunar orbit ballistic capture or more propulsive?":




                          From the NASA Space Science Data Coordinated Archive entry on Hagoromo,




                          A solid propellant (KM-L) retrorocket with a mass of 4 kg was mounted inside the spacecraft for orbit insertion.





                          @DavidHammen's answer to the question "How could tiny Hagoromo have been seen visually from earth confirming its lunar orbit?" is a click away and worth the read, so I won't re-quote it here.



                          See both (either) linked question for more images of this kawaii spacecraft and it's "parent" craft.






                          share|improve this answer














                          Muses A Lunar Orbiter (Hagoromo)



                          above: from Gunter's Space Page




                          According to Gunter's Space Page's Muses A Lunar Orbiter (Hagoromo):




                          It was launched piggy-back on the Muses A (Hiten) probe into a highly elliptical Earth orbit which passed by the Moon ten times during the mission. At 19:37 UT on 18 March 1990 as Hiten approached its first lunar flyby, the small Hagoromo spacecraft was released into lunar orbit, making Japan the third nation to orbit the Moon. Although the S-band transmitter aboard Hagoromo had failed on 21 February 1990, the ignition of the Hagoromo deceleration rocket was confirmed by ground observation at 20:04:03 UT, the estimated orbit was 7400 × 20000 km with a period of 2.01 days. No contact could be established after orbit insertion.




                          @DavidHammen's answer to the question "Was Hagoromo's capture into lunar orbit ballistic capture or more propulsive?":




                          From the NASA Space Science Data Coordinated Archive entry on Hagoromo,




                          A solid propellant (KM-L) retrorocket with a mass of 4 kg was mounted inside the spacecraft for orbit insertion.





                          @DavidHammen's answer to the question "How could tiny Hagoromo have been seen visually from earth confirming its lunar orbit?" is a click away and worth the read, so I won't re-quote it here.



                          See both (either) linked question for more images of this kawaii spacecraft and it's "parent" craft.







                          share|improve this answer














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                          edited 13 mins ago

























                          answered 19 mins ago









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