diff --git a/Comanche055/TPI_SEARCH.agc b/Comanche055/TPI_SEARCH.agc
index 7179558..6cd84bb 100644
--- a/Comanche055/TPI_SEARCH.agc
+++ b/Comanche055/TPI_SEARCH.agc
@@ -30,30 +30,27 @@
 
 # Page 551
 # TPI SEARCH
-#
+
 # PROGRAM DESCRIPTION S17.1 AND S17.2
-#
+
 # FUNCTIONAL DESCRIPTION
-#
-# THE TPI SEARCH ROUTINE DETERMINES THE MINIMUM TOTAL VELOCITY TRANSFER TRAJECTORY FROM A GIVEN TPI
+
+# 	THE TPI SEARCH ROUTINE DETERMINES THE MINIMUM TOTAL VELOCITY TRANSFER TRAJECTORY FROM A GIVEN TPI
 # MANEUVER TIME WITHIN THE CONSTRAINT OF A SAFE PERICENTER.  THIS VELOCITY IS THE SUM OF THE IMPULSIVE VELOCITIES
 # FOR THE TPI AND TPF MANEUVERS.
-#
-# THE S17.1 ROUTINE EXTRAPOLATES THE STATE VECTORS OF BOTH VEHICLES TO THE TPI TIME AND COMPUTES THE
-# RELATIVE PHASE ANGLE BETWEEN THE VEHICLES, THE ALTITUDE DIFFERENCE (I.E., THE MAGNITUDE DIFFERENCE OF THE
+# 	THE S17.1 ROUTINE EXTRAPOLATES THE STATE VECTORS OF BOTH VEHICLES TO THE TPI TIME AND COMPUTES THE
+# RELATIVE PHASE ANGLE BETWEEN THE VEHICLES, THE ALTITUDE DIFFERENCE(I.E. THE MAGNITUDE DIFFERENCE OF THE
 # POSITION VECTORS) AND SELECTS A SEARCH SECTOR BASED ON THE SIGN OF THE ALTITUDE DIFFERENCE.
-#
-# THE S17.2 ROUTINE FURTHER DEFINES THE SEARCH SECTOR BY COMPUTING ANGULAR LIMITS AND USES THE TIME THETA
+# 	THE S17.2 ROUTINE FURTHER DEFINES THE SEARCH SECTOR BY COMPUTING ANGULAR LIMITS AND USES THE TIME THETA
 # SUBROUTINE TO COMPUTE THE SEARCH START AND END TIMES.  THE SEARCH IS THEN MADE IN AN ITERATIVE LOOP USING THE
 # LAMBERT SUBROUTINE TO COMPUTE THE VELOCITIES REQUIRED AT TPI TIME AND AT TPF TIME.  EXIT FROM THE SEARCH LOOP
 # IS MADE WHEN SOLUTION CRITERIA ARE MET (NORMAL EXIT) OR AS SOON AS IT IS EVIDENT THAT NO SOLUTION EXISTS IN
 # THE SECTOR SEARCHED.
-#
+
 # CALLING SEQUENCE
-#
+
 # 	BOTH ROUTINES ARE CALLED IN INTERPRETIVE CODE AND RETURN VIA QPRET.  S17.1 HAS ONLY A NORMAL EXIT.
-#	S17.2 RETURNS VIA QPRET FOR NORMAL EXIT AND TO ALARUMS FOR ERROR EXIT.
-#
+# S17.2 RETURNS VIA QPRET FOR NORMAL EXIT AND TO ALARUMS FOR ERROR EXIT.
 # SUBROUTINES CALLED
 #
 #	CSMCONIC
@@ -69,11 +66,11 @@
 
 		EBANK=	RACT3
 
-# **** TEMPORARY ****
+# 	**** TEMPORARY ****
 
 HPE		2DEC	157420.0 B-29		# EARTH'S MIN. PERICENTER ALTITUDE 85 N.M.
 
-HPL		2DEC	10668.0213 B-29		# MOON'S MIN. PERICENTER ALTITUDE 35000 FT.
+HPL		2DEC	10668.0213 B-29		# MOON:S MIN. PERICENTER ALTITUDE 35000FT
 
 CDSEC		2DEC	40000
 
@@ -301,7 +298,7 @@ JUNCT3		VLOAD
 		SL*
 			0,2
 		STORE	HP
-# ITSWICH DENOTES INTERPOLATION -- SOLUTION ACCEPTANCE IS FORCED
+# ITSWICH DENOTES INTERPOLATION--SOLUTION ACCEPTANCE IS FORCED
 		BON	DLOAD
 			ITSWICH
 			ENDEN
@@ -315,9 +312,9 @@ JUNCT3		VLOAD
 		BMN	DSU			# (HPLIM-HPO)-(HPLIM-HP)=HP-HPO
 			INTERP			# SOLUTION AT HAND
 		BMN	DLOAD
-			ALARUMS			# IT'S GETTING WORSE -- SOUND THE ALARM
+			ALARUMS			# IT'S GETTING WORSE - SOUND THE ALARM
 			CDSEC
-JUNCT1		BOFF	DCOMP			# OFF IS PLUS, ON IS MINUS
+JUNCT1		BOFF	DCOMP			# OFF IS PLUS ON IS MINUS
 			KFLAG
 			+1
 		STORE	DELTEE
@@ -386,7 +383,7 @@ ENDEN		VLOAD
 			RELDELV
 		SIGN	STADR			# NOW SIGN(RELDELV)=SIGN(SG2)
 		STCALL	RELDELV
-			TRANSANG		# COMPUTE OMEGA T, CENTRAL ANGLE
+			TRANSANG		# COMPUTE OMEGA T , CENTRAL ANGLE
 		VLOAD	DOT
 			RACT3
 # Page 558
@@ -417,8 +414,7 @@ NEXUS		STODL	NN1
 		COUNT	07/XANG
 
 # CENTRAL ANGLE SUBROUTINE
-#
-# THIS SUBROUTINE COMPUTES THE CENTRAL ANGLE OF TRAVEL OF THE
+# 	THIS SUBROUTINE COMPUTES THE CENTRAL ANGLE OF TRAVEL OF THE
 # PASSIVE VEHICLE DURING THE TRANSFER.
 
 TRANSANG	STQ	SETPD
@@ -435,9 +431,9 @@ TRANSANG	STQ	SETPD
 		PDVL	VSR*			# SQRT MU (+18 OR +15)			00D
 			RPASS4
 			0,2
-		ABVAL	PDDL*			# MAGNITUDE OF R 	(+29 OR +27)	02D
+		ABVAL	PDDL*			# MAGNITUDE OF R (+29 OR +27)		02D
 			MUTABLE,1
-		PDVL	VSQ			# 1/MU 			(+34 OR +28)	04D
+		PDVL	VSQ			# 1/MU (+34 OR +28)			04D
 			VVEC
 		NORM	DMPR			# PUSH LIST AT 02D
 			X1
@@ -445,12 +441,12 @@ TRANSANG	STQ	SETPD
 		DMP	SRR*
 			02D
 			0 	-3,1
-		BDSU				# R V**/MU 		(+6)
+		BDSU				# R V**/MU (+6)
 			D1/32
 		NORM	PDDL
 			X1			# (2 - R V**/MU) 	(+6-N)
 		SR1R	DDV			# MAGNITUDE OF R 	(+30 OR +28)
-		SL*	PUSH			# R/(2 - R V**/MU)	(+29 OR +27)	02D
+		SL*	PUSH			# R/(2 - R V**/MU)	(+29 OR +27)02D
 			0 	-5,1
 		SR1	SQRT
 		DMP
@@ -475,9 +471,9 @@ TRANSANG	STQ	SETPD
 
 # TPI SEARCH DISPLAY ROUTNE
 
-P17		TC	AVFLAGA			# AVFLAG = CSM, SET TRACK + UPDATE FLAGS
+P17		TC	AVFLAGA			# AVFLAG = CSM , SET TRACK + UPDATE FLAGS
 		TC	P17.1
-P77		TC	AVFLAGP			# AVFLAG = LEM, SET TRACK + UPDATE FLAGS
+P77		TC	AVFLAGP			# AVFLAG = LEM , SET TRACK + UPDATE FLAGS
 P17.1		TC	P20FLGON		#	SET UPDATE FLAG
 		CAF	V06N37			#	DISPLAY TTPI TIME
 		TC	VNP00H
@@ -487,15 +483,15 @@ P17.1		TC	P20FLGON		#	SET UPDATE FLAG
 			S17.1			# UPDATE STATE VECTORS TO TTPI
 		SET	AXT,1
 			UPDATFLG
-		DEC	2			# DELTA H = 2 K POSITIVE, KFLAG OFF
+		DEC	2			# DELTA H = 2	K POSITIVE , KFLAG OFF
 		BOFF	AXT,1
 			KFLAG
 			+2
-		DEC	1			# DELTA H = 1 K NEGATIVE, KFLAG ON
+		DEC	1			# DELTA H = 1	K NEGATIVE , KFLAG ON
 # Page 560
 		SXA,1	EXIT
 			OPTION2
-		CAF	V06N72			# DISPLAY PHI, DELTA H, SEARCH OPTION K
+		CAF	V06N72			# DISPLAY PHI , DELTA H , SEARCH OPTION K
 		TC	VNCOMP17
 		TC	INTPRET
 		CLEAR	SET
@@ -519,9 +515,9 @@ P17.2		STCALL	HPERMIN
 			S17.2
 		SET	EXIT
 			UPDATFLG
-P17.3		CAF	V06N58			# DISPLAY DELTA VTPI, DELTA VTPF, AND H
+P17.3		CAF	V06N58			# DISPLAY DELTA VTPI , DELTA VTPF , AND H
 		TC	VNCOMP17
-		CAF	V06N55			# DISPLAY PERICENTER CODE AND CENTRAL ANG,
+		CAF	V06N55			# DISPLAY PERICENTER CODE AND CENTRAL ANG.
 		TC	BANKCALL
 		CADR	GOFLASHR
 		TC	GOTOP00H		# TERMINATE PROGRAM
@@ -554,4 +550,3 @@ ALARUMS		SET	EXIT
 		TC	VNCOMP17
 		TC	GOTOP00H		# PROCEED ILLEGAL TERMINATE PROGRAM
 V06N72		VN	0672
-