The solid rocket propellant for the Space Shuttle (and Tomahawk Missiles) contain . ammonium perchlorate (NH4CIO4(s) ) . aluminum powder (Al(s) ) • bound together with polymer compound. The reaction that produces the engine thrust is: 6 NHẠCIO4(s) + 10 Al(s) + 4 Al203(5) + 2 AlCl3(s) + 12 H2O(g) + 3 N2(9) Data: MM (NHẠCIO4(s) = 117.49g/mol m (NHẠCIO4(s)) = 500.0 kg a) With an excess of aluminum powder (Al) and 500.0 kg of ammonium perchlorate (NH,CIO4() • how many moles (nH20 and nn2) of each of the two gases (H20(9) + N2(9) will be produced? n (H20(9) = 1 Select ] n (N2 (9)) = 1 Select ] b) At standard temperature and pressure (STP ~ 0.00 °C / 1.000 atm) • how many liters (VH20 and Vn2) of each of the two gases (H20(9) + N29)) will be produced from the reaction of the 500.0 kg of NH¼CIO4(s) With an excess of aluminum powder? Data: T = PV = nRT P = NH20 = nN2 = Calculate: (STP) V (H20(9) = | Select V (N2 (9)) = I Select | c) The exhaust temperature of the Space Shuttle is approximately 3500°C. What are the volumes of the two gases in this reaction at this temperature and pressure: (3500°C and 1.000 atm) PV1 / T1 = P2V2 / T2 Data: T(K) = P(atm) = Calculate: (3500°C and 1.000 atm) VH20 = I Select VN2 = | Select)
The solid rocket propellant for the Space Shuttle (and Tomahawk Missiles) contain . ammonium perchlorate (NH4CIO4(s) ) . aluminum powder (Al(s) ) • bound together with polymer compound. The reaction that produces the engine thrust is: 6 NHẠCIO4(s) + 10 Al(s) + 4 Al203(5) + 2 AlCl3(s) + 12 H2O(g) + 3 N2(9) Data: MM (NHẠCIO4(s) = 117.49g/mol m (NHẠCIO4(s)) = 500.0 kg a) With an excess of aluminum powder (Al) and 500.0 kg of ammonium perchlorate (NH,CIO4() • how many moles (nH20 and nn2) of each of the two gases (H20(9) + N2(9) will be produced? n (H20(9) = 1 Select ] n (N2 (9)) = 1 Select ] b) At standard temperature and pressure (STP ~ 0.00 °C / 1.000 atm) • how many liters (VH20 and Vn2) of each of the two gases (H20(9) + N29)) will be produced from the reaction of the 500.0 kg of NH¼CIO4(s) With an excess of aluminum powder? Data: T = PV = nRT P = NH20 = nN2 = Calculate: (STP) V (H20(9) = | Select V (N2 (9)) = I Select | c) The exhaust temperature of the Space Shuttle is approximately 3500°C. What are the volumes of the two gases in this reaction at this temperature and pressure: (3500°C and 1.000 atm) PV1 / T1 = P2V2 / T2 Data: T(K) = P(atm) = Calculate: (3500°C and 1.000 atm) VH20 = I Select VN2 = | Select)
Chemistry for Engineering Students
4th Edition
ISBN:9781337398909
Author:Lawrence S. Brown, Tom Holme
Publisher:Lawrence S. Brown, Tom Holme
Chapter5: Gases
Section: Chapter Questions
Problem 5.62PAE: 62 Ammonium dinitramide (ADN), NH4N(NO2)2, was considered as a possible replacement for aluminium...
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![The solid rocket propellant for the Space Shuttle (and Tomahawk Missiles) contain
· ammonium perchlorate (NHẠCIO4(s) )
. aluminum powder (Al(s) )
• bound together with polymer compound.
The reaction that produces the engine thrust is:
6 NHẠCIO4(s) + 10 Al(s)
4 Al203(5) + 2 AIICĪ3(s) + 12 H20(g) + 3 N2(g)
Data:
MM (NH4CIO4(s)) = 117.49g/mol
m (NH4CIO4(s) = 500.0 kg
a) With an excess of aluminum powder (Al) and 500.0 kg of ammonium perchlorate (NH4CIO4(s)
• how many moles (nH20 and nn2) of each of the two gases (H20(9) + N2(g)) will be produced?
n (H20(g)) =
[ Select )
n (N2 (9)) =
[ Select J
b) At standard temperature and pressure (STP ~ 0.00 °C / 1.000 atm)
• how many liters (VH20 and Vn2) of each of the two gases (H20(g) + N2(g)) will be produced from the reaction of the 500.0 kg of NH4CIO4(s) With an excess of aluminum powder?
Data:
T =
PV = nRT
P =
NH20 =
NN2 =
Calculate: (STP)
V (H20(9)) =
| Select )
V (N2 (9)) = 1 Select ]
c) The exhaust temperature of the Space Shuttle is approximately 3500°C.
What are the volumes of the two gases in this reaction at this temperature and pressure:
(3500°C and 1.000 atm)
P1V1 / T1 = P2V2 / T2
Data:
T(K) =
P(atm) =
Calculate: (3500°C and 1.000 atm)
VH20 =
[ Select )
VN2 =
[ Select )](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fb99220ad-d702-4943-b904-ec3abe399c73%2F08e171f8-ca84-4a65-a2a6-675a98056142%2Fxqj8tch_processed.png&w=3840&q=75)
Transcribed Image Text:The solid rocket propellant for the Space Shuttle (and Tomahawk Missiles) contain
· ammonium perchlorate (NHẠCIO4(s) )
. aluminum powder (Al(s) )
• bound together with polymer compound.
The reaction that produces the engine thrust is:
6 NHẠCIO4(s) + 10 Al(s)
4 Al203(5) + 2 AIICĪ3(s) + 12 H20(g) + 3 N2(g)
Data:
MM (NH4CIO4(s)) = 117.49g/mol
m (NH4CIO4(s) = 500.0 kg
a) With an excess of aluminum powder (Al) and 500.0 kg of ammonium perchlorate (NH4CIO4(s)
• how many moles (nH20 and nn2) of each of the two gases (H20(9) + N2(g)) will be produced?
n (H20(g)) =
[ Select )
n (N2 (9)) =
[ Select J
b) At standard temperature and pressure (STP ~ 0.00 °C / 1.000 atm)
• how many liters (VH20 and Vn2) of each of the two gases (H20(g) + N2(g)) will be produced from the reaction of the 500.0 kg of NH4CIO4(s) With an excess of aluminum powder?
Data:
T =
PV = nRT
P =
NH20 =
NN2 =
Calculate: (STP)
V (H20(9)) =
| Select )
V (N2 (9)) = 1 Select ]
c) The exhaust temperature of the Space Shuttle is approximately 3500°C.
What are the volumes of the two gases in this reaction at this temperature and pressure:
(3500°C and 1.000 atm)
P1V1 / T1 = P2V2 / T2
Data:
T(K) =
P(atm) =
Calculate: (3500°C and 1.000 atm)
VH20 =
[ Select )
VN2 =
[ Select )
Expert Solution
Step 1
Answer:
By the use of given balanced chemical equation we can convert the number of moles of Ammonium perchlorate into number of moles water and nitrogen. Later on those moles can be used for further calculation.
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